N653RW
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
DURING HEAVY CHECK FOUND CENTER FUSELAGE 3 AT FR 84/85, RT SEAT TRACK HAS CORROSION
DURING HEAVY CHECK FOUND AFT CARGO LOWER SKIN PANEL HAS 1EA CORRODED SHEAR CLIP AT FR 77, STGR 29L-29R
DURING HEAVY CHECK FOUND CRACK ON R/H WING LOWER SKIN OTBD OF RIB 4 DOUBLER
DURING HEAVY CHECK FOUND AFT CARGO LWR SKIN PANEL STRINGER 29R, FR 75-79 HAS NUMEROUS AREAS OF CORROSION.
STEER FAIL IN FLIGHT ON GEAR EXTENSION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND TO BE TRANSITORY CONDITIONS OF STEERING CONTROL MODULE.
LAVITORY STEP SLEEVE LEAKING AND FOUND 5 EA SHEAR CLIPS AND 1 INTERCOSTAL CORRODED BETWEEN FRA 85 TO 88 AND STR 27R TO 28R. REMOVED AND REPLACED 5 EA SHEAR CLIPS AND 1 INTERCOSTAL IAW EMB 170/175 SRM 51-41-01 AND 51-41-02. ALSO REF VP-045392-2025 N/R 15,16,17,23,25 FOR WORK ACCOMPLISHED.
LOUD AND CONTINUOUS HYDRAULIC THUMPING SOUND OCCURRING FROM NOSE GEAR AREA. THUMPING STARTED RIGHT AFTER GEAR RETRACTION AND CONTINUED UNTIL GEAR WAS EXTENDED. THUMPING WAS HEARD AND FELT AT 3-5 SECOND INTERVALS UNTIL THE GEAR WAS EXTENDED SEVERAL MINUTES LATER. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R UPLOCK PROXIMITY MLG (RH) SENSOR #2.
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE, AFT WASTE SERVICE BOX INTERNAL DOUBLER CORRODED. INTERNAL FUSELAGE, AFT WASTE SERVICE BOX INTERNAL DOUBLER HAS BEEN REPAIRED IAW EMB SRM 53-23-60, INTERNAL CUT OUT HAS BEEN NDT'D WITH NO FAULTS FOUND.
RH ENGINE AFT STRUT FAIRING, FRAME 7 CRACKED. REPLACED FRAME #7 IAW 51-43-04
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE CENTER SECTION III, LOWER FRAME 88 CORRODED FWD OF AFT LAV WASTE SERVICE PAN. INTERNAL FUSELAGE CENTER SECTION III, LOWER FRAME 88 REPLACED WITH NEW IAW EMB SRM 51-41-01.
DURING HEAVY CHECK MAINTENANCE FOUND INTERIOR FUSELAGE CENTER SECTION III, STRINGER 27R CORRODED AT STR END AT FR 88, FWD OF WASTE SERVICE PAN. INTERIOR FUSELAGE CENTER SECTION III, STRINGER 27R HAS BEEN REPAIRED BETWEEN FR88 AND 85 IAW EMB SRM 53-23-03 REPAIR 6. NDT REPORTS NO CRACKS FOUND.
** DURING HEAVY CHECK ** SHEAR CLIP FOUND CORRODED ON FR88 BETWEEN STR 27-28R. REPLACED SHEAR CLIP IAW SRM 51-41-02
R/H ELEVATOR O/B MOST RIB CRACKED. R&R'D RIB IAW SRM 51-43-02 PSE 55-10-017
DURING HEAVY CHECK MAINTENANCE FOUND LH HORIZONTAL STAB LEADING EDGE ROOT FAIRING HAS A CRACKED RIB. LH HORIZ STAB LEADING EDGE ROOT FAIRING RIB REPLACED IAW EMB SRM 51-41-01 AND SRM 51-43-04.
AFT CARGO SHEAR CLIP CORRODED AT FR85, STR 27R TO 28R. R&R'D SHEAR CLIP SRM 51-41-01 AND SRM 51-42-01 PSE 53-30-05
AFT CARGO SHEAR CLIP CORRODED AT FR. 86 STR 27L -28L. R&R'D SHEAR CLIP IAW SRM 51-41-01 & 51-41-02 PSE 53-30-05
AFT CARGO SHEAR CLIP CORRODED AT FR. 86 STR 27R -28R. R&R'D SHEAR CLIP IAW SRM 51-41-01 & 51-41-02 53-30-05
** DURING HEAVY CHECK ** SHEAR CLIP FOUND CORRODED ON FR89 BETWEEN STR 27-28R. REPLACED SHEAR CLIP IAW SRM 51-41-02
AFT CARGO, SHEAR CLIP CORRODED AT FR83 STR 28R -29R. R&R'D IAW SRM 51-41-01, 51-41-02 AND 51-43-01 PSE 53-23-05
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE CENTER SECTION III, SHEAR CLIP CORRODED ON FR88 BETWEEN STR 27-26R. INTERNAL FUSELAGE CENTER SECTION III, SHEAR CLIP REPLACED WITH NEW OF FR 88 BETWEEN STR 27-26R, CLIP INSTALLED IAW EMB SRM 51-41-01 AND 51-41-02.
AFT CARGO, SHEAR CLIP CORRODED AT FR83 STR 27R -28R. R&R'D IAW SRM 51-41-01, 51-41-02 AND 51-43-01 PSE 53-23-05
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE, CENTER SECTION III, SHEAR CLIP CORRODED ON FR87 BETWEEN STR 27-28R. INTERNAL FUSELAGE, CENTER SECTION III, SHEAR CLIP REPLACED WITH NEW ON FR87 BETWEEN STR 27-28R, CLIP INSTALLED IAW EMB SRM 51-41-01 AND 51-41-02.
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE, CENTER SECTION III, CORROSION ON FLOOR SUPPORT GUSSET PLATE ON FR90 RH IB SEAT TRACK. CORRODED FLOOR SUPPORT GUSSET PLATE ON FR90 RH IB SEAT TRACK REPLACED WITH NEW PART IAW SRM 51-41-02.
AFT CARGO SHEAR CLIP CORRODED AT FR 82 STR 28R TO 29R. REPLACED SHEAR CLIP IAW SRM 51-41-02 AND 51-41-03
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE, CENTER SECTION III, CORROSION FOUND ON FLOOR SUPPORT SHEAR PLATE BETWEEN FR87-88 AND BETWEEN RH/LH IB SEAT TRACKS. CORRODED FLOOR SUPPORT SHEAR PLATE BETWEEN FR87-88 AND BETWEEN RH/LH IB SEAT TRACKS REPLACED WITH NEW IAW SRM 51-42-01.
WHILE AIRCRAFT WAS IN HEAVY CHECK** INTERNAL FUSELAGE CENTER SECTION III CORROSION FOUND ON FLOOR SUPPORT GUSSET FR90 BETWEEN RHIB SEAT TRACK AND CROSS BEAM REPLACED WITH NEW PART IAW SRM 51-41-02
AFT CARGO, SHEAR CLIP CORRODED AT FR82, STR 27R TO 28R. R&R'D SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02, PSE 53-20-05
WHILE AIRCRAFT WAS IN HEAVY CHECK** AFT CARGO SHEAR CLIP @ FR 75 STR 29R TO 28R. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND SRM 51-41-02
DURING HEAVY CHECK MAINTENANCE FOUND INTERNAL FUSELAGE, CENTER SECTION III, CORROSION ON FLOOR SUPPORT SHEAR PLATE BETWEEN FR87-88 AND BETWEEN RH/LH IB SEAT TRACKS. CORRODED FLOOR SUPPORT SHEAR PLATE BETWEEN FR87-88 AND BETWEEN RH/LH IB SEAT TRACKS REPLACED WITH NEW IAW SRM 51-42-01.
INT FUSE, CENTER SECTION, CORROSION FOUND AT FLOOR SUPPORT R/H SHEAR PLATE BTW FR 87-88. R&R'D SHEAR PLATE IAW SRM 51-42-01 AND 51-42-02 PSE 52-23-05
R/H WING #3 SLAT FOUND CRACKED AT O/B SLAT TO TRACK FITTING. REMOVED AND REPLACED SLAT IAW 27-81-07-400-801-A
FWD CARGO SILL, 3RD CLIP FROM FRONT CORRODED @ STR 25R TO 26R. R&R'D CLIP PER SRM 51-41-01. PSE 53-21-009
DURING HEAVY CHECK MAINTENANCE FOUND RH HORIZONTAL STAB TIP RIB FOUND CRACKED. RH HORIZONTAL STAB TIP RIB REPLACED IAW SRM 51-46-02.
FWD FUSELAGE INTERIOR FRAME 16, SHEAR TIE FOUND CORRODED BTW STR 23-24L. R&R SHEAR TIE IAW SRM 51-41-02 & 51-41-01 PSE 53-10-16
RH LE AT SLAT #2, O/B TRACK, SKIN CUTOUT TRACK. REPAIRED CRACK PER SRM 51-23-04, 51-23-05 PSE 57-40-11
DURING HEAVY CHECK MAINTENANCE FOUND RH ENGINE PYLON OB AFT PYLON LINK BRACKET, IB FLANGE BUSHING MIGRATED. RH ENGINE PYLON OB AFT PYLON LINK REPAIRED IAW ETD2021-170-038270 AND SB170-54-0014 REV 2. NDT'D WITH NO CRACKS FOUND.
RH H-STAB MID RIB 10A (170-62571-001) AND 11A (170-62783-001) FOUND CRACKED. R&R'D RIBS PER REPUBLIC AIRWAYS 170EO- 55-0004 -1
PHOTOLUMINESCENT STRIP COVER DAMAGED AT 11CD. R&R STRIP IAW 33-51-07.
FWD LH EMERGENCY LIGHT POWER UNIT FAULT. R&R FWD LH EMERGENCY LIGHT BATTERY IAW AMM 33-50-01.
EMERGENCY LIGHT BATTERY FAULT. PERFORMED EMERGENCY LIGHTS POWER UNIT CHARGE PROCEDURE IAW AMM 33-50-01.
L1 DOOR WILL NOT DISARM OR OPEN. ADJUSTED L1 DOOR EVACUATION SLIDE FLOOR FITTINGS IAW AMM 52-10-21, OPS CHECK GOOD AT THIS TIME.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON FWD ATTACH SPLICE FOR PANEL 195NL. REMOVED AND REPLACED FWD ATTACH SPLICE FOR PANEL 195NL PER SRM 51- 40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RIB 12A INTERNALLY ON RH HORIZONTAL BETWEEN MID SPAR AND FRONT SPAR JUST AFT OF 4TH RIVET FROM FRONT SPAR UPPER RIVET ROW. REMOVED AND REPLACED RH HORIZONTAL RIB 12A REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON INNER FLANGE ON PANEL 192BL. REMOVED AND REPLACED INNER FLANGE FOR PANEL 192BL. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RIB 11A INTERNALLY ON RH HORIZONTAL BETWEEN MID SPAR AND FRONT SPAR JUST AFT OF 5TH RIVET FROM FRONT SPAR UPPER RIVET ROW. REMOVED AND REPLACED NEW RIB 11A ON RH HORIZONTAL REF. EMB SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III DRY AREA 53-23 RH SIDE REINFORCEMENT STRUCTURE AT FRAME 84. REMOVED AND REPLACED CENTER FUSELAGE III DRY AREA 53-23 R-H SIDE REINFORCEMENT STRUCTURE AT FRAME 84. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON SPLINES ON TORQUE TUBE NR 6 RH. REMOVED AND REPLACED R/H 6 TORQUE TUBE WITH NEW UNIT, REF: AMM 27-51-03. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RIB 12A INTERNALLY ON LH HORIZONTAL BETWEEN MID SPAR AND FRONT SPAR JUST AFT OF 4TH RIVET FROM FRONT SPAR UPPER RIVET ROW. REMOVED AND REPLACED RIB 12A ON LH HORIZONTAL REF SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT. REMOVED AND REPLACED RH AFT PANEL SUPPORT BETWEEN FRAMES 87-90 REFER SRM 51-40-08. APPLIED SURFACE PROTECTION TO AREA PER SRM 51-23-06. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RIB 11A INTERNALLY ON LH HORIZONTAL BETWEEN MID SPAR AND FRONT SPAR JUST AFT OF 5TH RIVET FROM FRONT SPAR UPPER RIVET ROW. PERFORMED PERMANENT REPAIR TO RIB 11A OF THE LH HORIZONTAL BY MEANS OF REMOVING DAMAGED ANGLES AND FABRICATING AND INSTALLING NEW ANGLES ONTO THE ORIGINAL RIB 11A IAW ETD 2019-107077 REV A. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON INNER FLANGE ON PANEL 192CR. REMOVED AND REPLACED INNER FLANGE ON PANEL 192CR, APPLIED SURFACE PROTECTION TO PANEL 192 CR PER SRM 51-23-06. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" AT FRAME 87 AROUND THE RIVETS. FABRICATED AND INSTALLED REPAIR DOUBLER FOR RH FLOOR BEAM BETWEEN FRAMES 87-88 PER SRM 53-23-10/ REPAIR 01P. APPLIED SURFACE PROTECTION TO AREA PER SRM 51-*23-05, 51-23-06. A/C REMAINS IN CHECK.
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 85; STR 28R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FR 85; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00.
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 87; STR 28R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FR 87; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 88; STR 28R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FR88; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00
DURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON AFT DRAIN MAST INTERNAL AFT LATERAL STIFFENER BETWEEN FR 86-87; STR 28R-27R. REMOVED AND REPLACED AFT DRAIN MAST INTERNAL AFT LATERAL STIFFENER BETWEEN FR 86-87 STGR 27R-28R. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 82; STR 28R. REMOVED AND REPLACED SHEAR CLIP AT FR 82; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND L1 DOOR LOWER BEAM REWORK CORROSION AT FWD AND AFT GIRT BAR FITTING ATTACHMENT AREAS. REMOVED AND REPLACED L1 DOOR LOWER BEAM. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 83; STR 28R. REMOVED AND REPLACED SHEAR CLIP AT FR 83; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 84; STR 28R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FR 84; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND CENTER FUSELAGE III INTERNAL- CORROSION ON SHEAR CLIP AT FR 86; STR 28R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FR 86; STR 28R. REF SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP AND FASTENERS REF EMB SRM 51-23-06 AND CPM 51-25-00
DURING HEAVY CHECK MAINTENANCE FOUND LH INBD (FLOOR) SEAT TRACK (P/N 170-67659-431)) FROM FR 23 TO FR34/43 HAS SPOTS OF GOUGES/CORROSION. CUT AND REMOVED SECTION OF LH INBD SEAT TRACK BETWEEN FR30-31 AND FABRICATED SPLICE DOUBLERS FOR SPLICE REPAIR AT FR30-34. RESTORED SURFACE PROTECTION TO NEW SPLICE SECTION AT FR 30-34 LH INBD SEAT TRACK, REF. SRM 51-23-06 CPM 51-25-00. ETD2019-170-107734. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND RH OTBD (SIDEWALL) SEAT TRACK (P/N 170-02056-006) FROM FR 34/43 TO 59/74 HAS SPOTS OF GOUGES/CORROSION. REMOVED AND REPLACED RH OTBD SEAT TRACK FR 34/43 TO 59/74, RESTORED SURFACE PROTECTION ON RH OTBD SEAT TRACK FR 34/43 TO 59/74, REF SRM 51-23-06, CPM 51-25-00. REF SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND RH INBD (FLOOR) SEAT TRACK (P/N 170-67660-431) FROM FR 23 TO 34/43 HAS SPOTS OF GOUGES/CORROSION. REMOVED AND REPLACED RH INBD (FLOOR) SEAT TRACK (P/N 170-67660-431) FROM FR 23 TO 34/-43 REF SRM 51-40-08. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND LH INBD (FLOOR) SEAT TRACK (P/N 170-86081-005)) FROM FR59/74 TO 84 HAS SPOTS OF GOUGES/CORROSION. REMOVED AND REPLACED LH INBD SEAT TRACK FROM FR74 TO 84 REF SRM 51-40-08. RESTORED SURFACE PROTECTION ON LH INBD FR74 TO 84 SEAT TRACK, REF SRM 51-23-06. CPM 51-25-00. A/C REMAINS IN CHECK.
DURING HEAVY CHECK MAINTENANCE FOUND LH INBD (FLOOR) 1ST CLASS SEAT TRACK (P/N 170-67307-001) FROM FR 20 TO FR30 HAS SPOTS OF GOUGES/CORROSION. REMOVED AND REPLACED LH INBD (FLOOR) 1ST CLASS SEAT TRACK FROM FR 20 TO FR30 PER SRM 51-40-08. RESTORED SURFACE PROTECTION TO LH INBD 1ST CLASS SEAT TRACK REF: SRM 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.
*WHILE IN HEAVY CHECK* MAINTENANCE FOUND LEVEL 2 CORROSION ON RH INBD (FLOOR) SEAT TRACK (P/N 170-86082-005)) FROM FR59/74 TO 84. MAINTENANCE REMOVED AND REPLACED RH INBD FLOOR SEAT TRACK BETWEEN FRAMES 59-84 PER SRM 51-40-08. APPLIED SURFACE PROTECTION TO FASTENERS PER SRM 51-23-05, 51-23-06.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON LAV SERVICE DOOR AT HINGE. REMOVED AND REPLACED LAV SERVICE DOOR. SRM 51-40-08. APPLIED SURFACE PROTECTION AND PLACARD LAV SERVICE DOOR PER SRM 51-23-04, 51-23-05, 51-23-06 AND AMM 20-10-09. A/C REMAINS IN CHECK.
RECIRC SMOKE MESSAGE. DECLARED EMERGENCY, DIVERTED, LANDED WITHOUT INCIDENT. R&R RECIRCULATION BAY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD.
SLAT DISAGREE MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND LH INBD (2/3) SKEW SENSOR TO BE OUT OF LIMITS. ADJUSTED SKEW SENSOR IAW AMM 27-83-01.
EMERGENCY BATTERY FAULT. R&R RT FWD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01.
FWD EMERGENCY LIGHT OVERHEAD INOP. RESECURED CONNECTOR IAW AMM 33-50-03.
MAINTENANCE REPORTED CORROSION ON THE GROUNDING POINT AT FRAME 90 AND STRINGER 19L. MAINTENANCE PERFORMED A MAJOR REPAIR IAW SRM 53-23-03, 51-41-01, 51-10-03, 51-40-04, 51-23-05, AND ETD2017-170-058047
MAINTENANCE REPORTED CORROSION ON THE SHEAR TIE AT FRAME 90. MAINTENANCE REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-02, 51-43-03, 51-40-02, & 51-31-00.
MAINTENANCE REPORTED CORROSION ON GALLEY FLOOR SPLICE PLATE AT RT SIDE FRAME 88. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR SPLICE PLATE AT RT SIDE FRAME 88 IAW SRM 51-75-16, 51-10-03, 51-40-02, & 51-23-06.
DURING HEAVY CHECK, FOUND CENTER SHEAR PANEL AT FRAME 88 CORRODED. MX REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-10-03, 53-23-10, 51-42-01, 51-40-03, AND 51-23-00.
CREW REPORTED THAT A SECTION OF EMERGENCY LIGHT STRIP WAS MISSING. MAINTENANCE REPLACED EMERGENCY LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT A PIECE OF EMERGENCY LIGHT STRIP WAS MISSING AT SEATS 1 C & D. MAINTENANCE FOUND INNER STRIP SLID AFT OF INSIDE COVER. MAINTENANCE REPOSITIONED AND SECURED EMERGENCY LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE FORWARD FLASHLIGHT HOLDER WAS BROKEN. MAINTENANCE R & R FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
CORROSION FOUND ON FWD CARGO AFT LOWER SEAL REST. R & R THE SEAL REST.
RT VERTICAL STAB SKIN IS CRACKED AT RIB 12 BELOW AND AFT OF THE HOIST FITTING. REPAIRED THE VERTICAL STABILIZER SKIN IAW ETD2015-170-051804.
CORROSION FOUND ON SHEAR TIE AT FRAME 27, STRINGERS 28L-28R. R & R THE SHEAR TIE. MAJOR REPAIR.
CORROSION ON THE LEFT SEAT TRACK, Y 10.748" AT FRAME 84. REPAIRED THE DAMAGE BY CUTOUT AND SPLICE REPAIR IAW ETD 2015-170-050804.
CORROSION FOUND ON THE SHEAR TIE AT FRAME 17, STRINGERS 25-26L. REMOVED, FABRICATED A NEW SHEAR TIE, AND INSTALLED.
CORROSION FOUND ON SHEAR TIE AT FRAME 28, STRINGERS 28L-28R. REMOVED, FABRICATED, AND REPLACED THE SHEAR TIE. MAJOR REPAIR
CORROSION FOUND ON THE FWD CARGO BEAM AROUND LATCH BOLT HOLES. R & R THE BEAM.
CORROSION ON THE FLOOR SUPPORT AT FRAMES 86 - 90. R & R THE FLOOR SUPPORT.
FOUND A CORRODED BRACKET. R & R THE BRACKET
FOUND AN ATTACH FLANGE CHAFED AND CORRODED AND MISSING TWO RECEPTACLES. R & R ATTACH FLANGE.
CORROSION FOUND ON THE FWD CARGO MIDDLE, LOWER SEAL REST. R & R THE SEAL REST.
CORROSION FOUND ON THE SHEAR TIE AT FRAME 17, STRINGERS 23-24L. R & R THE SHEAR TIE.
CORROSION FOUND ON SHEAR TIE AT FRAME 16, STRINGERS 27-28L. R & R THE SHEAR TIE.
CORROSION FOUND ON SHEAR TIE AT FRAME 16, STRINGERS 27-28R. R & R THE SHEAR TIE. MAJOR REPAIR.
RT WING STUB SPAR HAS THREE FASTENER HOLES SHOWING TWO CRACK INDICATIONS AT THE 5 AND 9 O'CLOCK POSITIONS AT THE FWD FACE OF THE HOLE. REPAIRED IAW ETD 2015-170-051845, REV A.
CORROSION FOUND ON THE AFT CARGO DOOR CUTOUT STRUCTURE LOWER BEAM FWD FINGER DOUBLER. BLENDED THE CORROSION, AND THE REMAINING MATERIAL WAS WITHIN LIMITS OF ETD 2015-170-052010.
CORROSION FOUND ON AFT CARGO DOOR CUTOUT STRUCTURE LOWER BEAM AFT FINGER DOUBLER. BLENDED CORROSION, REMAINING MATERIAL WITHIN LIMITS OF ETD 2015-170-052010.
CORROSION ON THE SHEAR TIE AT FRAME 17, STRINGERS 27-28L. R & R THE SHEAR TIE.
CORROSION FOUND ON SHEAR TIE AT FRAME 17, STRINGERS 27-28R. R & R THE SHEAR TIE.
CORRODED AND GOUGED AFT CARGO DOOR AFT SEAL REST. R & R THE SEAL REST.
CORROSION FOUND ON THE AFT CARGO FWD, LOWER SEAL REST. R & R THE SEAL REST.
CORROSION FOUND AT TWO PLACES, FRAME 84 BETWEEN SEAT TRACKS. REPAIRED DAMAGE BY CUT-OUT AND DOUBLER.
CORROSION WAS FOUND IN ONE SPOT AT FRAME 84 BETWEEN LT SIDE OF FUSELAGE AND LT SEAT TRACK. REPAIRED BY CUTOUT AND DOUBLER.
FOUND THREE CORRODED ANGLES. R & R THE ANGLES.
CORRODED AND GOUGED FWD CARGO CLOSEOUT. R & R THE CLOSE OUT PANEL.
CORROSION FOUND ON THE RIGHT GUSSET PLATE AT FRAME 90. R & R THE GUSSET.
CORROSION FOUND ON THE RIGHT Y +10.748" UPPER SHEET AT FRAMES 85-86. R & R THE UPPER SHEET.
CORROSION ON THE CENTER SPLICE AT FRAME 90. R & R THE SPLICE.
CORROSION FOUND ON THE RIGHT CENTER GUSSET PLATE AT FRAME 90. R & R THE GUSSET.
CORROSION FOUND ON THE RT FLOOR SUPPORT AT FRAME 84. R & R THE FLOOR SUPPORT.
CORROSION FOUND ON RIGHT FWD FLOOR SUPPORT BETWEEN FRAMES 12-14. R & R THE FLOOR SUPPORT.
CORROSION FOUND ON FWD CARGO FWD LOWER SEAL REST. R & R THE SEAL REST.
CABIN ALTITUDE HIGH ON CLIMBOUT IAW QRH, DEPLOYED MASKS. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT, FERRIED. R & R ALL BUT 2 EA O2 GENERATORS, OPS CHECK GOOD.
L2 DOOR NOT INDICATING THE "ARMED" POSITION IN DISPLAY WINDOW ON DOOR. ADJUSTED ARMED INDICATOR ON L2 DOOR IAW AMM 52-12-00.
STEERING FAILED EICAS MESSAGE WHEN LANDING GEAR WAS EXTENDED AT 2500 FEET. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED A/C RESET, NO MESSAGES PRESENT. FOUND CONNECTOR SLIGHTLY LOOSE ON NOSE LT PROXIMITY SENSOR. RESEATED CONNECTOR PLUG, PERFORMED OPS CHECK OF NLG, NO FURTHER DEFECTS NOTED.
AT FL 210, DOOR PAX AFT OPEN EICAS MESSAGE. L2 SHOWING OPEN, ALL OTHER INDICATIONS NORMAL. R & R L2 DOOR PROXIMITY SENSOR IAW AMM 52-72-21. OPS CHECK GOOD.
R2 DOOR WILL NOT ARM. R & R R2 DOOR FLEX BALL CABLE IAW S170EO-52-41-0003 AND AMM 52-42-40. OPS CHECKED GOOD.
DURING CRUISE FLIGHT AT FL 360, EICAS MESSAGE "DOOR PAX AFT OPEN" STATUS PAGE INDICATED L2 DOOR OPEN. ALL INDICATIONS ON DOOR WERE NORMAL AND MESSAGE EXTINGUISHED IN LESS THAN 1 MINUTE. R & R L2 DOOR INDICATION HARNESS IAW MM 52-72-21. OPS CHECK GOOD.
WHILE AT CRUISE AT FL 350, RECEIVED AN EICAS MESSAGE "DOOR PAX AFT OPEN" WITH RED INDICATION FOR L2 DOOR ON MFD STATUS PAGE. FOLLOWED QRH, CABIN PRESSURE NORMAL. VERIFIED GREEN DOOR CLOSED INDICATORS ON DOOR. MESSAGE PERSISTED REST OF FLIGHT. CLEANED AND OPS CHECKED L2 DOOR INDICATION, IAW AMM 52-72-21.
L2 DOOR, OPEN IN FLIGHT INDICATION. CLEANED L2 PAX DOOR SENSOR SPRINGS IAW AMM 53-23-04. ALL DOOR INDICATIONS OPERATE NORMALLY.
AT 32,000 FT, RECEIVED THE EICAS MESSAGE FOR AFT SERVICE DOOR OPEN. FOLLOWED CHECKLIST AND VERIFIED INDICATIONS WERE NORMAL. MESSAGE EXTINGUISHED BEFORE LANDING. CLEANED AFT PAX DOOR CLOSE SENSOR SPRING IAW AMM 53-23-04. OPS CHECKED GOOD.
F/A FOUND A LARGE PIECE OF EMERGENCY LIGHT MISSING. R & R NEW LIGHT STRIP IAW MM 33-50-21.
ROW 3 LT SIDE PHOTOLUMINESCENT STRIP LOOSE/DETACHED. REATTACHED STRIP IAW AMM 33-50-21.
EMERGENCY LIGHTS ON, IN ARMED POSITION. RESET CIRCUIT BREAKER FOR EMERGENCY BATTERY HEATER IAW SWPM 20-35-01, NO FURTHER DEFECTS NOTED.
FLAPS DID NOT EXTEND ON APPROACH. CREW DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FERRIED TO IND. REMOVED AND REINSTALLED SF-ACE NR 1 IAW AMM 27-53-02. PERFORMED ELECTRICAL RIG AND SYSTEM OPS TEST IAW AMM 27-50-00. OPS CHECK GOOD.
FLIGHT ATTENDANT REPORTS SULFUR TYPE SMELL IN CABIN DURING ALL PHASES OF FLIGHT. THE SMELL WAS CONSISTENT, DID NOT GET ANY WORSE OR ANY BETTER. PERFORMED OPS CHECK OF BLEED SYSTEM AND PACKS IAW AMM 36-00-00. NO FAULTS FOUND. INSPECTED OVERHEAD BINS, FOUND FOUL ODOR FROM BINS ROW 15. CLEANED OVERHEAD BINS IAW AMM 20-00-00.
DURING CLIMB THROUGH FL320 AN UNUSUAL AIRCRAFT BUFFETING WAS NOTICEABLE. AFTER LEVEL OFF, THE BUFFET WAS STILL PRESENT AND SLOWING IN AIRSPEED MADE BUFFETING MORE AGGRESSIVE. NO ABNORMAL INDICATIONS WERE NOTED. DIVERTED TO CMH, DECLARED EMERGENCY. REMOVED AND REPLACED FWD WTB FAIRING, DUCTS, BOOTS, AND CONNECTING RODS TO PACKS.
MCD GIRT BAR DID NOT RELEASE. REMOVED AND REPLACED L1 DOOR EMERGENCY EVACUATION SLIDE ASSY IAW AMM 25-65-01.
RED AND BLUE WIRE ON LEFT GREEN INDICATOR ON 2R DOOR, BEHIND PLASTIC IN FRONT OF INDICATOR. SECURED WIRING ON R2 DOOR IAW EMB 170 MM 52-42-00.
HYD 2 LOW QTY MESSAGE IN FLIGHT, QTY DROPPED TO 2 PERCENT. DIVERTED TO IND, DECLARED EMERGENCY. LANDED UNEVENTFULLY. FOUND RIGID PRESSURE LINE BEHIND IDG OIL COOLER LEAKING. REMOVED AND REPLACED CRACKED E2 HYD PRESS PIPE FROM EDP TO PYLON, NO LEAKS NOTED.
NOSE GEAR WOULD NOT RETRACT, CYCLED LANDING GEAR LEVER PER QRH, GOT 3 DOWN GREEN. LANDED WITHOUT INCIDENT. AFTER LANDING FOUND NLG DID NOT EXTEND PROPERLY CAUSING BOTH WHEELS TO COME INTO CONTACT WITH FWD NLG DOORS. REMOVED AND REPLACED BOTH NOSE WHEEL TIRES, RT AND LT FWD NLG DOORS AND ROD ASSEMBLIES IAW MM 32-22-01 AND 32-22-02, AND LANDING GEAR LEVER ASSEMBLY IAW MM 32-33-01 AND PERFORMED NLG SHOCK STRUT SERVICING IAW JOBCARD S12-12-09-600-801A. OPS CHECKED GOOD.
LEVEL 2 CORROSION POTABLE WATER SERVICE PANEL BOX, BOTH HORSE SHOW RETAINERS. REMOVED AND REPLACED RETAINERS IAW EMB 170 SRM 51-43-02.
LEVEL 2 CORROSION RHIB SEAT TRACK ON CF I, AREA ALSO GOUGED. REMOVED AND REPLACED RHIB SEAT TRACK IN CF I IAW EMB 170 SRM 51-43-01 AND 51-43-02.
CREW DIVERTED TO MCO DUE TO HYD SYS NR 1 LOW QUANTITY MESSAGE WITH QUANTITY SHOWING AT 15 PERCENT. CREW DID NOT DECLARE AN EMERGENCY. HYDRAULIC RESERVOIR NR 1 LEAKING, ECOLOGY BOTTLE OVERFLOWING. SERVICED HYDRAULIC SYSTEM NR 1 IAW EMB MM 12-12-01. CREW TAXIED OUT AND RETURNED TO GATE DUE TO HYD SYSTEM NR 1 FLUID WENT FROM 62 TO 20 PERCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SYSTEM RESERVOIR IAW EMB 170 MM 29-11-08.
CORROSION ON CROSSBEAM INTERCOSTAL PANEL AT FR19 LT SIDE. REMOVED AND TREATED MINOR CORROSION IAW EMB 170 SRM 51-12-01 AND 51-23-00.
CORROSION ON RT CROSS BEAM INTERCOSTAL PANEL AT FR17. REMOVED AND TREATED MINOR CORROSION IAW EMB 170 SRM 51-12-01 AND 51-23-00.
CORROSION ON RT CROSSBEAM INTERCOSTAL PANEL AT FR14. REMOVED AND TREATED MINOR CORROSION IAW EMB 170 SRM 51-12-01 AND 51-23-00.
CORROSION ON CROSSBEAM INTERCOSTAL PANEL AT FR16. REMOVED AND TREATED MINOR CORROSION IAW EMB 170 SRM 51-12-01 AND 51-23-00.
LOWER RT SEAT TRACK BEAM HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED RT SEAT TRACK IAW EMB 170 SRM 51-41-00, 51-43-00, 51-43-02.
EMERGENCY LIGHTS STAYED ON AFTER TEST. RESET POWER IAW EMB 170 MM 33-00-00. NO WRITE UPS SINCE.
ON TAXI OUT FROM THE GATE, CREW RECEIVED AN ADS 2 HEATER FAULT EICAS MESSAGE FOLLOWED BY AN ELECTRICAL SMOKE SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO GATE. MAINT FOUND WIRES TO THE TAT 2 PROBE BURNED AND PINS MELTED. THE TAT2 SENSOR, CONNECTOR PLUG AND ADSP4 PROBE WERE REPLACED. TAT 2 PROBE PN 102AW1AF.
FLIGHT 7763 DEN TO AUS - CREW REPORTS AFTER TAKEOFF AT ABOUT 100 FEET AGL RECEIVED THREE CAUTION MESSAGES: SHAKER ANTICIPATED, AOA LIMIT FAIL, WIND SHEAR FAIL. RETURNED TO FIELD. CREW ALSO REPORTS VERY STRONG HEADWINDS AND OR WAKE TURBULENCE FROM A UNITED A320 THAT TOOK OFF JUST AHEAD OF THEM. MAINTENANCE ACCOMPLISHED DOWNLOAD AND CHECKED FOR FAULT CODES AND REPORTS HEAVY GUSTY WINDS IN AREA. AIRCRAFT POWER WAS RESET AND ALL MESSAGES CLEARED.
FLT 7631 IAD TO IND, NR 1 ENG FALLING SHORT OF COMMANDED POWER WITH A LAG IN THROTTLE RESPONSE. SHUT DOWN ENGINE, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. ON INSPECTION, FOUND VARIABLE GUIDE VANE ACTUATOR TURNBUCKLE FAILED. REMOVED AND REPLACED NR 1 ENGINE.