N121HQ
Registered owner: REPUBLIC AIRWAYS INC, IN (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
EMERGENCY LIGHT BATTERY FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 2.
AILERON CABLE FAIRLEAD SHEAR CLIP AT FR22 HAS ENLARGED HOLES.REMOVED AND REPLACED 2EA AILERON CABLE FAIRLEAD SHEAR CLIPS PER SRM 51-40-08.
AILERON CABLE FAIRLEAD SHEAR CLIP AT FR22 HAS ENLARGED HOLES. REMOVED AND REPLACED 2EA AILERON CABLE FAIRLEAD SHEAR CLIPS PER SRM 51-40-08.
CORROSION ON INTERNAL SKIN BETWEEN FRAME 90/91 STRG 29R/28R. REMOVED AND REPLACED INTERNAL DOUBLER REF EMB ETD2021-170-039289 RESTORE FINISH REF EMB SRM 51-23-04, 51-23-05 & 51-23-06 ON SKIN. MAJOR REPAIR.
CORROSION ON WASTE BOX DOUBLER AFT OF FR88, O/B OF STR 28R. MAJOR REPAIR. REMOVED, LOCATED, DRILLED, AND ALODINED NEW WASTE BOX DOUBLER. INSTALLED NEW WASTE BOX DOUBLER. REF. SRM 53-23-60, 51-23-06, 51-40-02, 51-23-04, 51-40-08.
CORROSION NOTED AT STRG 28R BETWEEN FRAME 86 AND 87 AFTER REMOVAL OF SHEAR CLIP. REMOVED OF CORROSION AT STRG 28R BETWEEN FRAME 86 AND 87 FOUND TO BE OUT OF GEOMETRICAL TOLERANCE. LOCATED, DRILLED AND INSTALLED NEW STRINGER, NEW SHEAR CLIP AT 28R-29R AND SPLICES FROM FR 86-90. REF. ETD2021-170-038842-A (P/N: 170-85163-001)
FR 80-81 STGR 28R HAS CORROSION AROUND LIGHTNING HOLE OB SIDE. REMOVED CORRODED FR 80-81 STGR 28R BEAM. REF: SRM 51-40-08. INSTALLED NEW FR 80-81 STGR 28R BEAM. REF: SRM 51-40-08 PN# 170-66280-001. APPLIED SURFACE PROTECTION ON FR 80-81 STGR 28R BEAM. REF: SRM 51-23-05 AND 51-23-06
CORROSION ON SHEAR CLIP FR82 BETWEEN STGR 27R/28R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
CORROSION ON SHEAR CLIP FR 81 BETWEEN STRG 27R / 28R. REMOVED AND REPLACED SHEAR CLIP PN: 170-66885-001 REF EMB SRM 51-40-08, RESTORE FINISH REF EMB SRM 51-23-05 & 51-23-06. MAJOR REPAIR
CORROSION ON SKIN AFTER REMOVAL OF INTERCASOTAL, AREA OF HOT DRAIN MAST. REMOVED AND REPLACED INTERNAL HOT DRAIN MAST DOUBLER PER SRM 51-40-05
CORROSION ON SHEAR CLIP FR 90 BETWEEN STGR 28R AND 29R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
CORRODED SHEAR CLIP AT FRAME 90, STGR 29R - 28R. REMOVED SHEAR CLIP AT FRAME 90, STGR 29R - 28R REF SRM 51-40-08 CORRECTIVE ACTION INSTALLED NEW SHEAR CLIP AT FRAME 90, STGR 29R - 28R REF SRM 51-40-08 APPLIED PRIMER, TOP COAT AND CIC REF EMB SRTM 51-23-05, 51-23-06, CPM 51-25-00 . EVALUATED SHEAR CLIP AT FRAME 90 STGR 29R - 28R REF SRM 51-403 AND FOUND SHEAR CLIP TO HAVE 100% MATERIAL LOSS.
CORROSION ON INTERCOSTAL FWD OF HOT DRAIN MAST INTERNAL SIDE OF FUSELAGE FROM FR 86 - 87 STGR 26R - 25R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAME 86-87 BETWEEN STRINGER 26R-25R REF SRM 51-40-08. SEE WIPS AND TASKS FOR WORK PERFORMED
CORROSION ON INTERCOSTAL AFT OF HOT DRAIN MAST INTERNAL SIDE OF FUSELAGE FROM FR 86-87 STGR 26R - 25R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAME 86-87 BETWEEN STRINGER 26R - 25R REF SRM 51-40-08.
CORRODED SHEAR CLIP AND HARDWARE AT FR 87 , STGR 27R - 28R AS MARKED. CORRODED SHEAR CLIP AND HARDWARE AT FR 87 , STGR 27R - 28R AS MARKED. EVALUATED SHEAR CLIP AND HARDWARE AT FR 87, STGR 27R -28R REF SRM 51-40-03AND FOUND SHEAR CLIP TO HAVE 100% MATERIAL LOSS. EVALUATED SHEAR CLIP AND HARDWARE AT FR 87, STRGR 27R - 28R REF SRM 51-10-08T FR 87 DRILLED NEW SHEAR CLIP AT FR 87 , STGR 27R - 28R REF SRM 51-40-08. APPLIED PRIMER, TOPCOAT AND CIC REF EMB SRM 51-23-05,51-23-06, CPM 51-25-00
CORRODED SHEAR CLIP AT FR 76, STGR 29R -29L AS MARKED. REMOVED AND REPLACED SHEAR CLIP AT FR 76, STGBR 29R - 29L REF : EMB 175 SRM 51-40-08
CORRODED SHEAR CLIP AND HARDWARE AT FR 88, STGR 27R - 28R AS MARKED. REMOVED AND REPLACED SHEAR CLIP AT FR - 88 OTBD OF STGR 28 REF SRM 51-40-08. INSTALL WAS COMPLIED WITH ON WO H8297 SN 688.
PARKING BRAKE NOT RELEASED EICAS MESSAGE IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R EMERGENCY/PARKING BRAKE PRESSURE SWITCHES 1 AND 2. OPERATIONS CHECK GOOD.
ONE EMERGENCY EXIT SIGN IN BACK AND ONE ABOVE ROW 17 GOING OFF AND ON DURING TEST. CHARGED BATTERIES, OPERATIONS CHECK GOOD, IAW AMM 33-50-00.
DOOR R2 ARM VENT FLAP LEVER VERY DIFFICULT TO ACTUATE. CLEANED AND LUBED R2 ARM VENT FLAP, OPS CHECK GOOD.
L2 EMERGENCY SLIDE PARTIALLY DEPLOYED. R&R L2 DOOR SLIDE PER AMM 25-65-01 AND FLEX BALL CABLE PER R170EO-52-10-0001.
WHILE IN HEAVY CHECK - WASTE SERVICE PANEL INTERNAL SIDE HAS CORROSION AROUND LATCHES. REMOVED AND REPLACE WASTE SERVICE DOOR REF AMM 20-10-01.
WHILE IN HEAVY CHECK - RT HORIZONTAL STABILIZER RIB 11 CRACKED BETWEEN FRONT AND MID SPAR AT SECOND TO LAST FASTENER FROM THE FRONT AS MARKED. REMOVED AND REPLACED RIB 11A RT HORIZONTAL STABILIZER REF SRM 51-40-08.
WHILE IN HEAVY CHECK - WHILE PERFORMING L2 DOOR LOWER BEAM REWORK, CORROSION FOUND ON UPPER FLANGE AREA. REMOVED AND REPLACED NEW L2 DOOR LOWER BEAM, REF SRM 51-40-08. APPLIED TOP COAT TO L2 LOWER BEAM, REF SRM 51-23-06,
WHILE IN HEAVY CHECK - CORROSION ON FR 84, RT SIDE CROSSBEAM. PERFORMED PERMANENT REPAIR OF UPPER FLANGE OF CROSSBEAM 84 ON RT SIDE BY WAY OF FABRICATION AND INSTALLATION OF L ANGLE DOUBLER REPAIR IAW ETD2019-170-121697.
WHILE IN HEAVY CHECK - LT HORIZONTAL STABILIZER RIB 12 CRACKED BETWEEN FRONT AND MID SPAR AT 4TH AND 5TH FASTENERS FROM THE FRONT AS MARKED. REMOVED AND REPLACED LT HORIZONTAL STABILIZER RIB 12A REF SRM 51-40-08.
WHILE IN HEAVY CHECK - LT HORIZONTAL STABILIZER RIB 11 CRACKED BETWEEN FRONT AND MID SPAR AT 5TH FASTENER FROM THE FRONT AS MARKED. REPAIRED LT HORIZONTAL STABILIZER RIB 11 BY CUT OUT AND INSTALLATION OF L-ANGLE REPAIR PER ETD2019-170-124594.
WHILE IN HEAVY CHECK - CORROSION-AFT WET AREA FLOOR STRUCTURE LT SHEAR PANEL FR87-88. REMOVED AND REPLACED LT SHEAR PANEL FR87-88 REF SRM 51-40-08,
WHILE IN HEAVY CHECK - CORROSION-AFT WET AREA FLOOR STRUCTURE RT SHEAR PANEL FR87-88. REPLACED AFT WET AREA FLOOR STRUCTURE RT SHEAR PANEL FR87-88 IAW SRM 53-23-10/AD03.
WHILE IN HEAVY CHECK - CORROSION AT FR 88 - FR 89 RT SIDE OF FUSELAGE AS MARKED. REPLACED RT SILL WITH NEW FR 88-89 AND RESTORED FINISH REF SRM 51-75-16, 51-40-08, 51-40-02 AND 51-23-06.
R2 DOOR "DISARMED" INDICATION IS NOT SHOWING IN WINDOW. ADJUSTED ARM/DISARM LINKAGE. OPS CHECK GOOD IAW AMM 52-42-22.
L1 PNEUMATIC ASSY READS 0 PSI. R & R L1 DOOR DIAPHRAGM IAW AMM 52-11-53.
CORRODED SHEAR TIE, FRAME 90, STRINGER 28R. REMOVED, FABRICATED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01, AND ETD2017-170-052758.
CORROSION ON SHEAR TIE AT FRAME 90 BETWEEN STRINGERS 27R- 29L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORRODED SHEAR TIE AT FRAME 89, STRINGER 29R. INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01.
CORROSION ON SHEAR TIE AT FRAME 90, STRINGER 28L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORROSION ON SHEAR TIE AT FRAME 89 BETWEEN STRINGERS 29R - 29L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-02.
CORRODED STRINGER 29L SPLICE AT FRAME 91. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-43-04, 51-41-01, AND 51-42-02.
CORROSION ON SHEAR TIE, FRAME 90 BETWEEN STRINGERS 29L- 27R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORROSION FOUND ON THE SHEAR TIE AT FRAME 90 BETWEEN STRINGERS 29L - 27R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
STRINGER 28R SPLICE CORRODED AT FRAME 91. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-41-02 , 51-41-01, AND 51-43-04.
FOUND CORROSION ON SUBFRAME LOCATED BETWEEN FRAME 90 AND THE PRESSURE BULKHEAD, STRINGER 27L TO 27R. REPAIREDIAW ETD2017-170-051290.
CORROSION ON STRINGER 29L BETWEEN FRAMES 85-87, IN THE AFT CARGO. REPAIRED THE STRINGER AIW ETD2017-170-051673.
CORROSION ON AFT HOT WATER DRAIN MAST DOUBLER BETWEEN FR 86-FR 87 IN AFT CARGO. REMOVED AND REPLACED AFT HOT WATER DRAIN MAST DOUBLER AND ATTACHING SUPPORT ANGLES. REF SRM 51-41-02 SEE EAMS W/O H5690 SEQ 1645 SN 515 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON STR 29R BETWEEN FR 85-88 IN AFT CARGO. PERFORMED SPLICE REPAIR OF STR 29R ON P/N 170-91888-003 SEE EAMS W/O H5690 SEQ 1648 SN 518 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON STRINGER 29L, BETWEEN FRAMES 85-87, IN THE AFT CARGO BAY. REPAIRED IAW ETD2017-170-051673.
CORROSION ON WASTE SERVICE DOOR EXTERIOR OF FUSELAGE. REMOVED AND REPLACED WASTE ACCESS DOOR.
CORROSION ON INTERNAL SKIN BETWEEN FRAMES 85 - 88, STRINGER 29L - 29R. PERFORMED DOUBLER REPAIR IAW ETD2017-170-051866.
CORRODED ON SHEAR TIE AT FRAME 81 BETWEEN STRINGERS 27R - 28L. REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORRODED SHEAR TIE AT FRAME 89, BETWEEN STRINGERS 27R & 28R, R & R THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORODED SHEAR TIE AT FRAME 88, BETWEEN STRINGERS 27R & 28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, & 51-41-02.
CORRODED SHEAR TIE AT FRAME 87, BETWEEN STRINGERS 27L & 27R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORRODED SHEAR TIE AT FRAME 86, BETWEEN STRINGERS 27L- 27R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORRODED SHEAR TIE FRAME 85, BETWEEN STRINGERS 27R AND 27L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORRODED SHEAR TIE, FRAME 84 BETWEEN STRINGERS 27R AND 27L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORROSION ON THE SHEAR TIE AT FRAME 83, BETWEEN STRINGERS 27R & 27L REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORROSION ON THE SHEAR TIE AT FRAME 82 BETWEEN STRINGERS 27R AND 27L IN THE AFT CARGO BAY. REPLACED THE SHEAR TIE IAW 51-41-01, AND 51-41-02.
LEFT WING SYSTEM 1 HYDRAULIC LINE HAS LOOSE B-NUT WHERE IT PASSES THRU SPAR LL WING BOX AREA. REMOVED HYDRAULIC SYSTEM NR 1 LINES WHERE THEY PASS THRU SPAR 3 NEAR RIB 4 AT WING BOX AREA. REMOVED DAMAGE TO SPAR 3 BY DRILLING. FABRICATED BUSHING AND INSTALLED. REINSTALLED HYDRAULIC LINES. REF E175 SRM 57-50-05 AND SEE EAMS W/O H5690 SEQ 5506 SN 386 FOR WORK DETAILS.
CORROSION ON FRAME 16 DOUBLER. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02.
STANDOFF AT FRAME 16. CORRODED. REMOVED AND REPLACED THE STANDOFF IAW SRM 51-43-03.
CORRODED STAND OFF AT FRAME 17. REMOVED AND REPLACED THE STAND OFF IAW SRM 51-43-03.
CORRODED FLOOR SUPPORT, FRAMES 88 - 89. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01, & 51-42-01.
GOUGED AND CORRODED RT CENTER SEAT TRACK BETWEEN FRAME 22 - 23 AND FRAMES 34 - 43.. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-43-03 AND 51-43-04.
CORROSION ON AFT CARGO FLOOR SUPPORT BRACKET AT FR 80 STR 28R. REMOVED AND REPLACED P/N 170-87229-001 SEE EAMS W/O H5690 SEQ 1540 SN 221 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON SKIN INTERNAL FR 89-90 STR 27-28. PERFORMED DOUBLER REPAIR REF ETD2017-170-051466 ON P/N 170-91883-005 SEE EAMS W/O H5690 SEQ 1555 SN 260 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON STRINGER 28R, FRAMES 89-90. PERFORMED STRINGER SPLICE REPAIR IAW ETD2017-170-051673.
CORROSION ON SUPPORT STABILIZER AT FR 81 STR 28R IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED P/N 170-85686-002 SEE EAMS W/O H5690 SEQ 1544 SN 230 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON INTERNAL DOUBLER OF PANEL 192BR. BLENDED THE DOUBLER AND FOUND WITHIN LIMITS IAW SRM 51-76-16 RESTORE BACK TO ORIGINAL FINISH IAW 51-23-04, 51-23-05, AND 51-23-06.
CREW RECEIVED A L2 DOOR OPEN INDICATION. PRESSURIZATION WAS NOT LOST AND AN EMERGENCY WAS NOT DECLARED. MAINTENANCE PLACED ON MEL IAW AMM AND ACFT IS GOOD FOR SERVICE.
DURING HEAVY CHECK, RT SEAT TRACK AT +10.748 AT FRAME 84 IS CORRODED. MAINTENANCE PERFORMED PERMANENT REPAIR, REF ETD 2015-170-111552, ETD 2014-170-061394, SRM 53-00-10.
DURING HEAVY CHECK, WAS REPORTED THAT AFT CARGO CLOSE OUT PANEL IS CORRODED. MAINTENANCE R & R AFT CARGO CLOSE OUT PANEL IAW SRM 51-21-01, AMM 20-10-01, PN 170-67115-002 CLOSE OUT PANEL.
DURING HEAVY CHECK, FWD SEAL REST AT FWD CARGO DOOR THRESHOLD NUTPLATES ARE CORRODED. MAINTENANCE R & R FWD SEAL REST AT FWD CARGO DOOR THRESHOLD IAW SRM 51-23-04, 51-40-02, 51-23-06, PN 170-66803-401 SEAL REST.
DURING HEAVY CHECK, FWD FINGER DOUBLER AT FWD CARGO DOOR THRESHOLD. MAINTENANCE THE R & R FINGER DOUBLER IAW SRM 51-40-02, 51-40-02,
DURING HEAVY CHECK, AFT SEAL REST AT FWD CARGO DOOR NUTPLATES ARE CORRODED. R & R AFT SEAL REST AT FWD CARGO DOOR IAW SRM 51-40-02, 51-23-04, PN 170-66803-402, SEAL REST.
DURING HEAVY CHECK, WAS REPORTED THAT AFT FINGER DOUBLER AT FWD CARGO DOOR THRESHOLD IS CORRODED. MAINTENANCE R & R THE FINGER DOUBLER IAW SRM 51-42-02, 51-43-04.
DURING HEAVY CHECK, FWD CARGO DOOR SEAL REST AROUND NUT PLATES AT FWD CARGO DOOR THRESHOLD IS CORRODED. MAINTENANCE R & R FWD CARGO DOOR SEAL REST IAW SRM 51-41-01, 51-23-06, 51-41-02, 51-23-04. PN 170-66804-401, SEAL REST.
DURING HEAVY CHECK, THE SHEAR TIE AT FRAME 82 BETWEEN STRINGERS 26-27R IS CORRODED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-41-01, 51-40-02.
DURING HEAVY CHECK, WAS REPORTED THAT INTERNAL DOUBLER OF FUSELAGE PANEL 192CR IS CORRODED. MAINTENANCE R & R INTERNAL DOUBLER OF FUSELAGE PANEL 192CR IAW SRM 51-41-02, 51-23-05. PN 170-13414-004 SPACER.
DURING HEAVY CHECK, FLOORBOARD SUPPORT AT FRAME 80 BETWEEN STRINGERS 26-27 RT IS CORRODED. MAINTENANCE R & R FLOORBOARD SUPPORT AT FRAME 80 BETWEEN STRINGERS 26-27 RT IAW SRM 51-41-01, 51-40-02, 51-23-04. PN 170-87229-001 SUPPORT.
DURING HEAVY CHECK, RT FLOOR TRACK FRAME 12-20 IS CORRODED. MAINTENANCE R & R RT FLOOR TRACK FRAME 12-20 IAW SRM 51-41-01, 51-41-02, 51-41-03,51-43-04, PN 170-03264-001, TRACK.
DURING HEAVY CHECK, LT SEAT TRACK AT FRAME 19 IS CORRODED. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER IAW SRM 53-10-10, REPAIR 1.
DURING HEAVY CHECK FLOOR FITTING FOR OTBD AFT FWD LAV ATTACH POINT IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.
DURING HEAVY CHECK WAS REPORTED THAT SHEAR TIE AT FRAME 87 BETWEEN STRINGERS 27-28R IS CORRODED. MAINTENCE R & R THE SHEAR TIE IAW SRM 51-44-01, 51-40-02.
DURING HEAVY CHECK, WASTE SERVICE ACCESS DOOR IS CORRODED. MAINTENANCE R & R WASTE SERVICE ACCESS DOOR IAW AMM 5303-00.
DURING HEAVY CHECK, RT PANEL SUPPORT FRAME 86-90 IS CORRODED. MAINTENANCE R & R RT PANEL SUPPORT FRAME 86-90 IAW SRM 51-42-01, 51-40-00, 51-43-03, PN 170-86181-005, SUPPORT.
DURING HEAVY CHECK, RT FLOOR SILL FRAME 84 IS CORRODED. MAINTENANCE R & R RT FLOOR SILL FRAME 84 IAW SRM 51-23-04, 51-21-02, 51-41-02, 51-41-02, 51-43-02, 51-23-03, 51-23-06.
DURING HEAVY CHECK, RT OTBD SPLICE PLATE BETWEEN FRAMES 87-88 IS CORRODED. MAINTENANCE R & R RT OTBD SPLICE PLATE BETWEEN FRAMES 87-88 IAW SRM 51-42-02, PN 17065644-001, SPLICE.
DURING HEAVY CHECK, LT OTBD SPLICE PLATE BETWEEN FRAMES 87-88 IS CORRODED. MAINTENANCE R & R LT OTBD SPLICE PLATE BETWEEN FRAMES 87-88 IAW 51-42-02, 51-40-02, 51-42-01, PN 17065644-001 SPLICE.
DURING HEAVY CHECK, RT FLOOR SUPPORT FRAME 84 CORRODED. MAINTENANCE R & R RT FLOOR SUPPORT FRAME 84 IAW SRM 51-23-04, 51-21-02,51-41-02, 51-41-01 51-43-02, PN 170-65644-001, SILL.
DURING HEAVY CHECK WAS REPORTED THAT RT OTBD SPLICE PLATE BETWEEN FRAMES 87-88. MAINTENANCE R & R RT OTBD SPLICE PLATE BETWEEN FRAMES 87-88 IAW SRM 51-42-02. PN 17065644-001, SPLICE.
DURING HEAVY CHECK, WAS REPORTED THAT LT OTBD SPLICE PLATE BETWEEN FRAMES 87-88. MAINTENANCE R & R LT OTBD SPLICE PLATE BETWEEN FRAMES 87-88 IAW SRM 51-42-01. PN 17065644-001, SPLICE PLATE.
DURING HEAVY CHECK, RT CENTER SPLICE, FRAME 89 IS CORRODED. MAINTENANCE R & R RT CENTER SPLICE FRAME 89 IAW SRM 51-43-03, PN 170-86125-001, SPLICE.
DURING HEAVY CHECK, LT -10.748 UPPER SHEET AT FRAME 85-86 IS CORRODED. MAINTENANCE R & R LT -10.748 UPPER SHEET AT FRAME 85-86 IAW SRM 51-41-01, 51-53-03, PN 170-86101-001, UPPER SHEET.
DURING HEAVY CHECK, RT GUSSET PLATE AT FRAME 90 IS CORRODED. MAINTENANCE R & R RT GUSSET PLATE AT FRAME 90 IAW SRM 51-40-02, 51-23-04, 51-21-02, P/N 170-60259-001, GUSSET PLATE.
DURING HEAVY CHECK, LT SEAT TRACK -10.748 IS CORRODED. MAINTENANCE REPAIRED IAW ETD 2015-170-=111522 LT SEAT TRACK, -10.748 IAW SRM 53-00-10, ETD 2014-170-061394.
DURING HEAVY CHECK, BRACKET ON INTERIOR SIDE OF LAV SERVICE BOX IS CORRODED. MAINTENANCE R & R BRACKET ON INTERIOR SIDE OF LAV SERVICE BOX IAW SRM 51-42-02. PN 170-87889-401, BRACKET.
DURING HEAVY CHECK, SHEAR CLIP AT FRAME 88, STRINGER 27-28, RT IS CORRODED. MAINTENANCE R & R SHEAR CLIP AT FRAME 88, STRINGER 27-28, RT IAW SRM 51-41-01, 51-23-04, 51-41-02, 51-23-06, 51-23-05, PN 170-66531-001 SHEAR CLIP.
DURING HEAVY CHECK, BELLY SKIN INTERIOR SIDE FROM 28L-27R BETWEEN FRAMES 90-91 IS CORRODED. MAINTENANCE PERFORMED PERMAMENT REPAIR OF BELLY SKIN INTERIOR SIDE FROM 28L-27R BETWEEN FRAMES 90-91 BY A DOUBLER REPAIR, REF ETD 2015-170-114409.
DURING HEAVY CHECK, STUB WING SPAR 3 SHOWS CRACK LIKE INDICATIONS AT THE FASTENER REPLACEMENT. MAINTENANCE REAMED HOLE UNTIL NO CRACK-LIKE INDICATIONS, .547 INSTALLED BUSHING IAW ETD 2015-170-110996-A.
CREW REPORTED THAT THE CAPTAINS FLASHLIGHT WAS NOT CHARGING. MAINTENANCE R & R CAPTAINS FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE NR 2 ENGINE ROLLED BACK TO 27 PERCENT N1. AT 1000 FT, THE AUTOTHROTTLE TURNED OFF AND A MASTER CAUTION WARNING APPEARED. CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT. WITH EMERGENCY VEHICLES ROLLING, CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FMU IAW AMM AND OPS CHECKED GOOD.
CREW NOTED THAT THE NR 2 ENGINE WAS NOT PRODUCING FULL POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES IAW AMM WITH NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.
CREW REPORTED THAT THE AFT F/A FLASHLIGHT WAS MISSING CLIP. MAINTENANCE R & R AFT F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE FORWARD FLIGHT ATTENDANT FLASHLIGHT WOULD NOT CHARGE. R & R THE FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE FWD F/A FLASHLIGHT WAS NOT TAKING A CHARGE. MAINTENANCE INSTALLED FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN RT FUEL TANK, AROUND FLANGE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN RT FUEL TANK. MX R & R LINE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON RT WING TANK FUEL PIPE. MX R & R FUEL PIPE.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN RT FUEL TANK ON AND AROUND FLANGE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN LT WING. MX R & R FUEL LINE IAW AMM 20-10-13.
DURING HEAVY CHECK, FUEL PIPE CORRODED IN LT WING. MX R & R LT WING FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, LT WING CORROSION ON FUEL PIPE. MX R & R FUEL LINE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN LT WING. MX R & R FUEL PIPES IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN RT FUEL TANK IAW AMM 20-10-13. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION WAS FOUND ON FUEL LINE IN RT TANK. MX R & R FUEL LINE IAW AMM 20-10-13.
DURING HEAVY CHECK, FOUND AFT GALLEY TO HAVE MULTIPLE AREAS OF CORROSION. REMOVED CORROSION ON AFFECTED AREAS SRM 51-12-01, FABRICATED TRIM IAW SRM 51-31-00.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL LINE IN LT FUEL TANK. MX R & R FUEL LINE.
DURING HEAVY CHECK, CORROSION WAS FOUND ON FUEL LINE IN LT TANK ON AND AROUND FLANGE. MX R & R FUEL LINE.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE AROUND FLANGE LT WING. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN RT FUEL TANK. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE. MX R & R FUEL PIPE IN RT FUEL TANK. IAW AMM 20-10-13.
DURING HEAVY CHECK , CORROSION FOUND ON FUEL PIPE FOR RT WING FUEL TANK. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, RT FUEL TANK PIPE HAS CORROSION ON AN AROUND FLANGE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, RT FUEL TANK PIPE HAS CORROSION ON AN AROUND FLANGE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE. MX R & R FUEL LINE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION FOUND ON FUEL PIPE IN RT WING AROUND FLANGE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, CORROSION WAS FOUND ON FUEL PIPE IN RT TANK, ON AND AROUND FLANGE. MX R & R FUEL PIPE IAW AMM 20-10-13.
DURING HEAVY CHECK, RIB SUPPORT ANGLE BRACKET FWD SIDE OF LT WHEEL WELL CRACKED NEAR AILERON FEEL UNIT. MX R & R LT RIB 52 ANGLE IAW SRM51-40-02, 51-43-01, 51-21-05 SEE CONTINIUATION CARD, VP-036178-2013/430, C1 FOR DETAILS OF WORK PERFORMED, PN 170-30709-001, SUPPORT. AIRCRAFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.
DURING HEAVY CHECK, LT WING NR 5 FLAP TOQUE TUBE OTBD END CORRODED AT GEAR BOX. MX R & R NR 5 FLAP TORQUE TUBE IAW EMB 27-51-03, PN 5912949-2, FLAP TORQUE TUBE.
DURING HEAVY CHECK, LT WING FLAP TORQUE TUBE NR 6 INBD END CORRODED AT GEARBOX. MX R & R NR 6 FLAP TORQUE TUBE IAW AMM 27-51-03. PN 5912949-3 TORQUE TUBE. ACFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.
DURING HEAVY CHECK, RT WING NR 5 FLAP TORQUE TUBE OTBD CORRODED AT GEARBOX. MX R & R NR 5 FLAP TORQUE TUBE IAW AMM 27-51-03. PN 5912949-2 TUBE NR 5. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.
DURING HEAVY CHECK, ECS DUCTING SUPPORT BRACKETS ARE CRACKED ON LT FUSELAGE. MX R & R CRACKED SUPPORT BRACKET IAW SRM 51-41-01, PN 170-92986-001 SUPPORT. AIRCRAFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.
DURING HEAVY CHECK, REPORTED RT WING NR 6 FLAP TORQUE TUBE INBD END CORRODED AT GEAR BOX. MX R & R NR 6 FLAP TORQUE TUBE IAW AMM 27-51-03.
DURING HEAVY CHECK, RT HORIZONTAL STAB LEADING EDGE RIB CRACKED AT UPPER FLANGE. MX REPAIRED RIB 4 IAW ETD 2013-170-051888, SEE CONTINUATION CARD VP 036178-2013/0293 C1 FOR WORK PERFORMED. THIS REPAIR REPAIR DOES NOT REPRESENT A AIRWORTHINESS LIMITATION AND THE INSPECTION IN THE CURRENT MPG/MRBR IS SUFFICIENT.
DURING HEAVY CHECK, LEFT SEAT TRACK CORRODED AFT WET AREA. MX R & R SEAT TRACK IAW SRM 51-41-01, 51-43-01.
DURING HEAVY CHECK, RT WING OTBD FLAP CARRIAGE FWD MOUNT BOLT HAS A CORRODED NUT. MX R & R FWD MOUNT BOLT AND NUT IAW AMM 57-57-31.
DURING HEAVY CHECK, RT SEAT TRACK EXTENSION CORRODED IN AFT WET AREA. MX R & R RT SEAT TRACK IAW SRM 51-40-02, 51-42-01, 51-43-03.
DURING HEAVY CHECK, RT AFT PYLON ADEL CLAMPS, STANDOFFS,AND HARNESS CLAMPS CORRODED. MX R & R CORRODED STANDARDS IAW SRM 51-42-00, SWPM 20-51-00 AND AMM 20-10-03.
DURING HEAVY CHECK, L2 DOOR SLIDE ATTACH BRACKETS HAVE CORRODED BOLT. MX R & R BOLTS AS REQUIRED IAW AMM 52-12-40.
DURING HEAVY CHECK, L1 DOOR KEEPER CORRODED. MX R & R L1 DOOR KEEPER IAW AMM 53-10-21.
DURING HEAVY CHECK, FRAME 90 RT GUSSET PLATE FOUND CORRODED. MX R & R RT GUSSET PLATE IAW SRM 51-41-02, SHEET C-1 FOR ACCOMPLISHED. PN 170-60257-001, GUSSET. ACFT REMAINS AT UNTIL HEAVY CHECK IS COMPLETED.
DURING HEAVY CHECK, FRAME 90 LT SIDE GUSSET FOUND CORRODED. MX R & R LT GUSSET IAW SRM 51-41-02, SHEET C-1 FOR WORK ACCOMPLISHED, PN 170-60257-001 GUSSET. AIRCRAFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.
DURING HEAVY CHECK, L1 DOOR EMERGENCY SLIDE LOWER MOUNTING HARDWARE ON DOOR FOUND CORRODED. MX R & R MOUNTING HARDWARE IAW AMM 52-11-40.
CREW REPORTED THAT THE FWD F/A FLASHLIGHT WAS MISSING. MX REPLACED FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT UPON APPROACH, THEY RECEIVED A "FLAP FAIL" MESSAGE. ABORTED LANDING TO RUN QRH. HAD FLAPS 2 AND SLATS 3. DECLARED AN EMERGENCY. LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MX FOUND BOTH THE LT FLAP T3 AND T4 SKEW SENSORS HAD FAILED. MX R & R BOTH IAW AMM AND OPS CHECKED GOOD.
CREW REPORTS THAT THE FIRST OFFICERS FLASHLIGHT IS DIM. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER EMB AMM 33-51-0 AND OPS CHECKED GOOD.
CREW REPORTED, RECEIVED AN EMERGENCY BRAKE NOT RELEASED MESSAGE IN FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT, BRAKES OPERATED NORMALLY. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCHES PER EMB AMM.
CREW REPORTED L1 DOOR HARD TO DISARM AND INDICATION WINDOW ISNâT SHOWING ALL GREEN. MAINTENANCE CLEANED AND LUBED PASSENGER DOOR LOCK ASSY PER EMB 175 MM 52-12-5.
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION AROUND WASTE BOX. MAINTENANCE REMOVED AND REPLACED DOUBLER IAW EMB 175 SRM 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION AROUND WASTE BOX. MAINTENANCE REMOVED AND REPLACED DOUBLER IAW EMB 175 SRM 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FR 14 FLOOR CROSSBEAM , CORROSION OUTBD OF RT INBD SEAT TRACK BEAM. MX REPAIRED CORRODED AREA WITH RIVET IAW ETD 2012-170-001327A P/N FLUSH HEAD RIVET NAS1097-4. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION. THIS IS A MAJOR.
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE SHEAR WEB AFT OF L1 DOOR ON FWD CLOSET MOUNT BOLT HOLE. MAINTENANCE REMOVED AND REPLACED SHEAR WEB (DOUBLER FLOOR) AFT OF THE L1 DOOR IAW EMB 175 SRM 51-41-02, 51-10-03, 51-40-02, 51-40-04 & 51-43-04. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
CREW REPORTED EMERGENCY LIGHT IN CEILING OVER ROW 3 WAS INOP. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM PER EMB AMM, OPS CHECK GOOD.
CREW REPORTED SLAT FAIL MESSAGE ON EICAS PAGE. CREW FOLLOWED QRH PROCEDURES AND DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DISPATCHED TO AIRCRAFT, TROUBLESHOOT AND REMOVED AND REPLACED LEFT SLAT 2-3 SKEW SENSOR. COMPLETED OPERATIONAL CHECKS. ALL OPERATIONAL CHECKS GOOD. RETURNED AC BACK TO SERVICE.