N815MD
Registered owner: UMB BANK NA TRUSTEE, UT (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
ON DEPARTURE OUT OF LGA WE HEARD A LOUD BANG ON ROTATION DURING CLIMB OUT, WE RECEIVED A BRK LT FAULT MSG AND WHEN WE EXTENDED THE GEAR, WE HAD A LG LEVER DISAGREE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED DAMAGED HYDRAULIC LINES, SIDE STAY, BRACKET, WHEEL/TIRE ASSY, WHEEL SPEED SENSOR HARNESS, AND DOWNLOCK SENSOR.
DURING HEAVY CHECK FOUND CF III, LOWER SKIN, SHEAR CLIP AT FR81, RBL 27-28 FOUND CORRODED.R&R CFIII LOWER SKIN SHEAR CLIP AT FR81, RBL27-28 WITH NEW CLIP, IAW SRM 51-41-01 & 51-41-02.
DURING HEAVY CHECK FOUND R&R CORRODED SHEAR CLIP AT FWD. FUSE, FR16, BET. STRG 27R-28R IAW SRM 51-40-08.
DURING HEAVY CHECK FWD.. FUSE, LOWER SKIN REINFORCEMENT BET. FR16-17, BET. STRG. 26-27R. FWD. R&R FUSE, LOWER SKIN REINFORCEMENT BET. FR.16-17R, BET STRG. 26-27R IAW SRM 51-41-02 PAR. 4-6
DURING HEAVY CHECK FOUND CF III, LOWER SKIN, SHEAR CLIP AT FR 85, RBL 27-28, FOUND CORRODED. R&R CF III, LOWER SKIN, SHEAR CLIP AT FR 85, RBL 27-28 WITH NEW CLIP IAW SRM51-41-02 & 51-41-01.
DURING HEAVY CHECK FWD FUSE, SHEAR CLIP AT FR.17, BET. STRG. 23R-24R, FOUND CORRODED.R&R SHEAR CLIP AT FWD. FUSE FR17, BET STRG.23R-24R, IAW SRM 51-40-08.
DURING HEAVY CHECK, FWD. FUSE, SHEAR CLIP AT FR17, BET. STRG.24R-25R, FOUND CORRODED. R&R CORRODED SHEAR CLIP AT FWD. FUSE, FR17, BET STRG.24R-25R IAW SRM 51-40-08.
FWD FUSE SHEAR CLIP AT FR 17 BTWN STGR27R-28R FOUND CORRODED. MX REPLACED SHEAR CLIP IAW SRM 51-40-08
FWD FUSE SHESAR CLIP AT FR 17 STGR 27L-28L FOUND CORRODED. MX REPLACED SHEAR CLIP IAW SRM 51-40-08.
DURING HEAVY CHECK MAINTENANCE FOUND CF1, OXYGEN SUPPORT AT FR23, BET STGR 19R- 21R FOUND CORRODED. CF1, OXYGEN SUPPORT AT FR23, BET STGR 19R- 21R REPLACED IAW SRM 51-41-01 PARA 4-6, SRM 51-43-03 PARA 4-5.
DURING HEAVY CHECK MAINTENANCE LH WING, FLAP TORQUE TUBE F8, IB UNIVERSAL JOINT FOUND TO HAVE PITTING CORROSION ON THE SPLINES FROM LACK OF GREASE. REMOVED AND REPLACED UNIVERSAL JOINT AT LH WING FLAP TORQUE TUBE F8 IB SIDE IAW EMB SRM 51-42-01.
FWD FUSE SHEAR CLIPS (2) AT FR 17 BTWN STGR 28R-28L FOUND CORRODED. MX REPLACED SHEAR CLIP IAW SRM 51-40-08.
FWD FUSE SHEAR CLIP AT FR 17 BTWN STGR 26R-27R FOUND CORRODED. MX REPLACED SHEAR CLIP IAW SRM 51-40-08.
DURING HEAVY CHECK MAINTENANCE FOUND CF 1 OXYGEN REINFORCEMENT WEB BET FR23- FR24, STGR 21R CORRODED. CF 1 OXYGEN REINFORCEMENT WEB BET FR23- FR24, STGR 21R WAS REPLACED IAW EMB SRM 51-40-08 PARA 5.
FWD FUSE SHEAR CLIP AT FR17 BTWN STGR 25R-26R FOUND CORRODED. MX REPLACED SHEAR CLIP IAW SRM 51-40-08.
FWD FUSE SHEAR CLIP AT FR 17 BTWN STGR 26L-27L FOUND CORRODED. MX REPLACED SHEAR CLIP IAW SRM 51-40-08
DURING HEAVY CHECK MAINTENANCE CF111, GUSSET PLATE AT FR90, RBL11 FOUND CORRODED. CF111, GUSSET PLATE AT FR90, RBL11 WAS REPLACED IAW EMB SRM 51-40-08 PARA 3.
DURING HEAVY CHECK MAINTENANCE FOUND CABIN FWD WET AREA IB RH SEAT TRACK RBL 12 BETWEEN FR12-FR23 WITH DEEP CORROSION. CABIN FWD WET AREA IB RH SEAT TRACK RBL 12 BETWEEN FR12-FR23 REMOVED AND REPLACED IAW SRM 51-40-08.
DURING HEAVY CHECK MAINTENANCE FOUND CABIN FWD WET AREA LH WEB BETWEEN FR13-FR16 WITH CORROSION. REMOVED SAND REPLACED CABIN FWD WET AREA LH WEB BETWEEN FR13-FR16 WITH NEW IAW SRM 51-41-02.
DURING HEAVY CHECK MAINTENANCE FOUND CF111, LH IB SEAT TRACK BET ,FR74-FR84 FOUND MULTIPLE SPOTS OF CORROSION AND A GOUGE. CF111, LH IB SEAT TRACK BET ,FR74-FR84REPLACED IAW SRM 51-40-08.
RH WING UPPER SKIN TE BTWN RIB 10-11 CRACK FOUND. MX REPAIRED IAW ETD 2025-170-001191****MAJOR****
DURING GROUND INSP FOUND BROWN WATER COMING FROM BELOW AFT CARGO AREA. UPON FURTHER INSP FOUND WASTE SERVICE BOX DRAIN TUBE CLAMP BROKEN. ALSO FOUND 2 EA SHEAR CLIPS CORRODED,WASTE SERVICE BOX DELAMINATED AND SKIN CORRODED. REMOVED AND REPLACED SHEAR CLIPS AND INSTALLED DOUBLER IAW EMB 170/175 SRM 51-41-01 AND 51-43-02. ALSO REF VP-003654-2023 FOR WORK PERFORMED.
DURING HEAVY CHECK MAINTENANCE FOUND FWD FUSELAGE FLOOR STRUCTURE R/H SILL CORRODED AT FR 12 TO FR 15, RBL 39. FWD FUSELAGE FLLOR STRUCTURE R/H SILL AT FR 12 TO FR15 RBL 39 REMOVED AND REPLACED IAW ERJ 170 SRM 53-10-11. FASTENERS INSTALLED IAW ERJ 170 SRM 51-43-04 AND SRM 51-41-02
CENTER SHEAR PLATE AT FR 87 TO 88 CORRODED. R&R IAW SRM 51-42-01 AND 51-43-01.
L/H SHEAR PLATE AT FR 87 TO 88 CORRODED. R&R IAW SRM 51-42-01.
DURING HEAVY CHECK MAINTENANCE FOUND CTR FUSE III, R/H SHEAR PANEL AT FR 87 TO FR 88 CORRODED. REPLACED R/H SHEAR PANEL AT FR87 TO FR88 CTR FUS III IAW ERJ-170 SRM 51-42-01, SRM 51-42-02 AND SRM 51-43-01.
FLOOR STRUCTURE R/H GUSSET PLATE AT FR 90. RBL 29 CORRODED. R7R IAW SRM 51-40-02.
R/H FLOOR SUPPORT AT FR 84, RBL 39 CORRODED. R&R IAW SRM 51-41-02 AND 51-41-01.
CF III CORROSION FOUND ON FUSELAGE SKIN UNDER DRAIN SHROUD BETWEEN FR 84-85 & STR 28L-28R. REPAIRED IAW SRM 53-23-01/AD03
FWD EBAY OPEN EICAS AFTER ROTATION ON TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED FWD EBAY AND RESET EBAY DOOR.
PHOTOLUMINESCENT STRIP IN ROWS 1A-2A AND 4DC-5DC CRACKED. R&R PHOTOLUMINESCENT STRIPS IN ROWS 1A-2A AND 4DC-5DC.
L1 DOOR STUCK CLOSED. REMOVED DEBRIS AND RE-ALIGNED GIRT BAR INTO L1 DOOR FITTING, IAW AMM 52-11-40.
FWD CABIN CEILING EMERGENCY LIGHT IS INOPERABLE. R & R ELPU 2 FUSE 2, IAW SAMM 33-50-01.
DURING THE CLIMB PHASE, A LOUD POP OCCURRED FOLLOWED BY AIR LEAK NOISE WITH CLIMBING CABIN ALTITUDE. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. ON THE GROUND, FWD EBAY DOOR FLUCTUATED FROM GREEN TO AMBER, BACK TO GREEN ON STATUS PAGE. R & R FWD AVNX ACCESS HATCH.
*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON CENTER FUSELAGE 3 CROSSBEAM UPPER FLANGE AT FR 87 AND RBL 12. CROSSBEAM WAS REPAIRED IAW ETD2019-170-124120. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** A CRACK WAS FOUND ON L1 DOOR SURROUND UPPER SEAL SEAT CORNER FR 16. SEAL SEAT WAS REPAIRED IAW ETD 2019-170-125326. AIRCRAFT RETURNED TO SERVICE.
*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON CENTER FUSELAGE 3 UNDER FLOOR FRAME STABILIZER CLIP AT STR18L FR 84. CLIP WAS REPLACED IAW SRM 51-41-01 AND ETD 2019-170-123637. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON CENTER FUSELAGE 3 FLOOR SUPPORT GUSSET PLATE AT FR 89 AND LBL 9. PLATE WAS REPLACED IAW SRM 51-42-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 FLOOR SUPPORT SPLICE AT L2 DOOR SURROUND FR 88. MX REPLACED CENTER FUSELAGE 3 FLOOR SUPPORT SPLICE PN 170-86107-001 AT L2 DOOR SURROUND FR 88 IAW SRM 51-43-03. AC REMAINS IN YQG FOR COMPLETION. SEE NRC# 4500442-1000-0047 FOR WORK DETAILS.
*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON L1 DOOR LOWER SILL BEAM @ FWD AND AFT GIRT BAR FITTING AREA. SILL BEAM WAS BLENDED AND FOUND WITHIN LIMITS PER SRM 53-10-11, GIRT BAR FITTINGS AREA REPAIRED IAW ETD 2019-170-123413. AIRCRAFT RETURNED TO SERVICE.
WHILE AC WAS IN FOR HVY CK FOUND CORROSION ON CENTER FUSELAGE 3 FLOOR SUPPORT SHEAR PANEL AT FR 88 AND LBL 9. MX REMOVED AND REPLACED CENTER FUSELAGE 3 FLOOR SUPPORT SHEAR PANEL PN 170-65927-007 AT FR 88 AND LBL 9 IAW SRM 51-42-01 AND ETD 2019-170-123840. AC REMAINS IN YQG FOR COMPLETION. SEE NRC 4500442-1000-0041 FOR WORK PERFORMED.
WHILE AC WAS IN FOR HVY CK CORROSION FOUND ON CENTER FUSELAGE 3 LONGITUDINAL FLOORBEAM AT FR 88 RBL 9. MX REPLACED PN 170-65669-004 CENTER FUSELAGE 3 LONGITUDINAL FLOORBEAM CLIP IAW SRM 51-43-01. AC REMAINS IN YQG FOR COMPLETION. SEE NRC # 4500442-1000-0045 FOR WORK DETAILS.
WHILE AC WAS IN FOR HVY CK FOUND CORROSION ON CENTER FUSELAGE 3 FLOOR SUPPORT SHEAR PANEL AT FR 88 AND LBL 9. MX REMOVED AND REPLACED PN 170-91919-001CENTER FUSELAGE 3 FLOOR SUPPORT SHEAR PANEL AT FR 88 AND LBL 9 IAW SRM 51-42-01. AC REMAINS IN YQG FOR COMPLETION. SEE NRC # 4500442-1000-0043 FOR WORK PERFORMED.
*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON CENTER FUSELAGE 3 UNDER FLOOR FRAME STABILIZER ANGLE AT SR 19R FR 85. ANGLE WAS REPLACED IAW SRM 51-43-03 AND ETD 2019-170-126371. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
WHILE AC WAS IN FOR HVY CK FOUND CORROSION ON CENTER FUSELAGE 3 FLOOR STRUCTURE PANEL SUPPORT. MX REMOVED AND REPLACED PN 170-86181-005 CENTER FUSELAGE 3 FLOOR STRUCTURE PANEL SUPPORT IAW SRM 51-42-01. AC REMAINS IN YQG FOR COMPLETION. SEE NRC# 4500442-1000-0044 FOR WORK PERFORMED.
WHILE AC WAS IN FOR HVY MX FOUND NICKS ON FUSELAGE EXT SKIN UNDER L2 DOOR SCUFF PLATE. MX REPAIRED SKIN PN 170-65121-005 IAW ETD2019-170-123338. FOR WORK PERFORMED SEE NRC # 4500442-2000-0031. AC RETURNED TO SERVICE.
WHILE AC WAS IN FOR HVY CHECK FOUND FWD AVIONICS ACCESS HATCH EXTERNAL SKIN HAS MINOR SCRATCH DAMAGE. MX REPAIRED FWD AVIONICS ACCESS HATCH EXTERNAL SKIN PN 170-00665-407 IAW ETD 2019-170-123339. SEE NRC# 4500442-2000-0030 FOR WORK PERFORMED. AC RETURNED TO SERVICE ON 9-22-19.
WHILE AC WAS IN FOR HVY CKS FOUND CRACK ON LT IB AFT FLAP FITTING. MX REMOVED AND REPLACED LT IB AFT FLAP FITTING PN 170-39187-001 IAW AMM 57-52-00-000-801-A. FOR DETAILS OF WORK PERFORMED SEE NRC# 4500442-5000-0003. AC WAS RETURNED TO SERVICE.
EMERGENCY LIGHT IN CENTER OF CABIN INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-50-01. OPS CHECKED GOOD.
RIGHT SHEAR PLATE FOUND CORRODED FR 87 - 88. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM-51-42-02.
LEFT COCKPIT FLOOR DOUBLER CORRODED, FRAMES 12 - 7. REMOVED AND REPLACED THE FLOOR DOUBLER IAW SRM 51-75-16 PN 170-03236-063. SEE EAMS W/O H5806 SN 402 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA
AFTER REMOVAL OF THE RT GUSSET AT FRAME 90, ADDITIONAL CORROSION WAS FOUND UNDERNEATH ON MONUMENT FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-41-01, AND 51-41-02.
COCKPIT CROSSBEAM AT FRAME 11, CORRODED IN CENTER. COMPLIED WITH ETD 2017-170-070737.
RIGHT COCKPIT FLOOR DOUBLER CORRODED, FRAMES 7 - 12. COMPLIED WITH ETD 2017-170-070791.
CENTER COCKPIT FLOOR DOUBLER CORRODED. FRAMES 10-7. REMOVED AND REPLACED THE FLOOR DOUBLER IAW SRM 51-75-16.
RIGHT INBD SEAT TRACK GOUGED AND CORRODED, FRAMES 43 - 59. REMOVED AND INSTALLED A NEW SEAT TRACK IAW SRM 51-40-02, 51-41-01, 51-42-01, 51-43-03, AND 51-43-04.
COCKPIT CROSSBEAM AT FRAME 11, CENTER GUSSET CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-41-02.
SHEAR TIE CORRODED, FRAME 76, STRINGERS 28 - 29R. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01.
CORROSION AT STRINGER 20R BETWEEN FRAME FRAMES 23 AND 24 . REMOVED AND REPLACED THE STRINGER IAW SRM 51-41-01, AND 51-43-03.
CORROSION ON THE AFT CARGO DOOR LOWER CENTER SEAL REST. REMOVED AND INSTALLED A NEW SEAL REST IAW SRM 51-41-01, 51-23-04, 51-23-05, AND 51-23-06.
CORROSION AFT SERVICE DOOR LOWER CENTER SEAL REST. REMOVED AND REPLACED THE SEAL REST IAW SRM 51-40-02.
SHEAR TIE CORRODED, FRAME 87, STRINGERS 27 - 28R. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
SHEAR TIE CORRODED FRAME 89, STRINGERS 26 - 27L. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01, AND SRM 51-41-02.
SHEAR TIE CORRODED FRAME 75, STRINGERS 28 - 29R. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01, AND 51-41-02.
CORROSION FWD BOTTLE SUPPORT BRACKET. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-41-01, & 51-41-02.
CORROSION ON THE FWD CARGO SHEAR TIE FRAME 16, STRINGERS 26 - 27R. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-43-03, 51-41-02, AND 51-41-01.
CORRODED INTERNAL DOUBLER ON PANEL 192CR. INSTALLED A NEW DOUBLER IAW SRM 51-40-02, SRM 51-40-02, SRM 51-23-04, SRM 51-23-05, SRM 51-23-06, AND SRM 51-40-04.
CORROSION ON THE FWD RT FLOOR DOUBLER, FRAMES 13 - 14. REMOVED AND REPLACED THE FLOOR DOUBLER IAW SRM 51-40-02, 51-23-05, 51-41-02, 51-42-04, AND 51-23-06.
CORROSION ON THE FWD LT OTBD LAVATORY MOUNT FRAME 16. REMOVED AND REPLACED LAVATORY MOUNT IAW SRM 51-43-04, AND 51-23-06.
CORROSION CREW OXYGEN BOTTLE LOWER SUPPORT, FR24 AND STR 20R. REMOVED AND INSTALLED NEW LOWER SUPPORT ARM AND PLATE AT FR23- FR24 STR 20R REF SRM 51-41-01, 51-43-03 AND 51-41-02 PN 170-87405-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON THE FWD RT CENTER GUSSET AT FRAME 84. REMOVED AND REPLACED THE GUSSET IAW SRM 51-23-06.
CORROSION RT SHEAR PNL FRAME 87/88. REMOVED AND REPLACED SHEAR PLATE PN: 170-91919-001 REF SRM 51-42-01. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION RT AFT FLOOR SUPPORT FRAME 88/90. REMOVED AND REPLACED PNL SUPPORT PN: 170-86181-005 REF SRM 51-43-03 & 51-42-01. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
RT OUTBD GUSSET CORRODED AS MARKED FR 90. REMOVED AND INSTALLED RT OUTBOARD GUSSET AT FR90 IN REF TO SRM51-40-01 PN 170-60259-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION FWD CARGO SHEAR CLIP AT FR17, STR 27L-28L. REMOVED AND INSTALLED NEW SHEAR CLIP REF SRM 51-41-01 & 51-41-02. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION ON THE FWD LT FLOOR SUPPORT, FRAMES 84-85. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01.
CORROSION FWD DRAIN MAST AFT ANGLE SUPPORT, INTERNAL SIDE OF FUSELAGE BETWEEN FR16-17, STR 26R-27R. REMOVED AND INSTALLED NEW FWD DRAIN MAST AFT SUPPORT ANGLE REF SRM SRM 51-43-03, 51-41-02, 51-41-01. PN 170-08185-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
LT INBD SEAT TRACK CORRODED AS MARKED FR 84. INSTALLED FABRICATED LT INBD SEAT TRACK FILLER AND SPLICE FR 83-84, REF SRM 53-00-10/REPAIR 01 PN 170-86081-005. AIRCRAFT REMAINS IN HEAVY CHECK BNA
RT GUSSET CORRODED AS MARKED FR 91. REMOVED AND REPLACED RT GUSSET PN: 170-60250-003 REF SRM 51-40-02, 51-23-04, 51-41-02. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
RT INTERCOSTAL CORRODED AS MARKED FR 90-91. REMOVED AND REPLACED RT INTERCOSTAL FR 90-91 REF SRM 51-43-03 PN: 170-60244-003. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
LT CENTER GUSSET CORRODED AS MARKED FR 90. REMOVED AND REPLACED LT CENTER GUSSET PN: 170-60261-001 REF SRM 51-40-02, 51-23-04, 51-41-02. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
RT MIDDLE GUSSET CORRODED AS MARKED FR 90. REMOVED AND INSTALLED RT MIDDLE GUSSET AT FR90 IN REF TO SRM51-40-01 PN 170-60257-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION FWD CARGO SHEAR CLIP AT FRAME 16 STRINGER 27R/28R. REMOVED AND REPLACED SHEAR CLIP PN: 170-03859-002 REF 51-41-01 AND 51-41-02. AIRCRAFT REMAINS IN HEAVY CHECK BNA
CORROSION ON THE RT FLOOR SUPPORT, FRAME 86. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, AND 51-43-03.
CORROSION FWD CARGO SHEAR CLIP AT FRAME 17 STR 27R/28R. REMOVED AND REPLACED SHEAR CLIP PN: 170-03335-001 REF SRM 51-41-01. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
MAIN CABIN DOOR ARMING LEVERS ARE DIFFICULT TO PUSH DOWN. ADJUSTED 4 DOOR ARMING LEVERS IAW AMM 52-12-52.
AFT GALLEY EMERGENCY EXIT SIGN WILL NOT ILLUMINATE WITH EMERGENCY LIGHTS TO ON. R&R AFT RT IB EMERGENCY POWER UNIT IAW AMM 33-50-01. ALL FAULTS CLEARED.
EMERGENCY LIGHT OVER ROW 6 INOPERATIVE. R & R FWD NR 1 EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECKED GOOD.
L2 DOOR NOT SHOWING GIRT BAR INDICATOR. RESECURED L2 DOOR BUSTLE COVER IAW MM 52-12-22.
F/AS REPORT VERY LOUD SQUEAL IN FLIGHT COMING FROM L2 DOOR, NEAR THE FLOOR, CAN BE HEARD AS FAR FWD AS ROW 9. ADJUSTED LOWER ROLLERS ON L2 DOOR REF AMM 52-12-00. OPS AND LEAK CHECK GOOD.
DURING INSPECTION, THE SPLICES FOR 170EO-53-10-0008, SB 170-53-0056, WERE FOUND TO BE INCORRECTLY INSTALLED. MAINTENANCE REMOVED AND CORRECTLY RE-INSTALLED THE SPLICES IAW ETD2015-170-100228.
DURING INSPECTION, CORROSION WAS FOUND ON THE RT INBD SEAT TRACK AT FRAME 82. MAINTENANCE R & R THE SEAT TRACK IAW SRM 53-23-10.
DURING INSPECTION, CORROSION WAS FOUND ON THE RT INBD SEAT TRACK AT FRAMES 52-54. MAINTENANCE R & R THE SEAT TRACK IAW SRM 51-40-02, 51-42-03, 51-43-04.
DURING INSPECTION, CORROSION WAS FOUND AT THE AFT INTERCOSTAL AT THE AFT HOT DRAIN. MAINTENANCE R & R THE AFTER INTERCOSTAL AT THE HOT DRAIN MAST IAW SRM 51-40-02, 51-21-02, 51-41-01, 51-41-02.
DURING INSPECTION, CORROSION WAS FOUND AT THE FORWARD INTERCOSTAL AT THE AFT HOT DRAIN. MAINTENANCE R & R THE FORWARD INTERCOSTAL AT THE AFT HOT DRAIN MAST IAW SRM 51-40-02, 51-21-02, 51-41-01, 51-41-02.
DURING INSPECTION, CORROSION WAS FOUND AROUND THE FASTENER HOLES ON THE AFT CARGO FORWARD AND AFT LOWER CORNER SEAL REST. MAINTENANCE R & R THE FORWARD AND AFT LOWER CORNER SEAL REST IAW SRM 53-23-29.
DURING INSPECTION, CORROSION WAS FOUND AT THE AFT PASSENGER DOOR THRESHOLD. MAINTENANCE R & R THE SUPPORT SEAL IAW SRM 51-41-01.
DURING INSPECTION, CORROSION WAS FOUND BETWEEN SEAT TRACKS AT FRAME 84. MAINTENANCE REPAIRED THE CORROSION IAW ETD2015-170-094057.
DURING INSPECTION, CORROSION WAS FOUND AT THE LEFT SPLICE PLATE AT FRAMES 87-88 AFT OF THE AFT PASSENGER DOOR. MAINTENANCE R & R THE SPLICE IAW SRM 51-42-02.
DURING INSPECTION, CORROSION WAS FOUND AT THE L2 THRESHOLD TIE STRAP AFT OF FRAME 85. MAINTENANCE R & R THE THRESHOLD TIE STRAP IAW SRM 51-43-01.
DURING INSPECTION, CORROSION WAS FOUND ON THE LT SEAT TRACK AT FRAME 84. MAINTENANCE REPAIRED THE DAMAGE IAW ETD2015-170-094033.
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER SPLICE AT FRAME 90. MAINTENANCE R & R THE SPLICE IAW SRM 51-23-04, 51-23-05.
DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SHEAR PLATE AT FRAMES 87-88. MAINTENANCE R & R THE SHEAR PLATE IAW SRM 51-40-02.
DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT CENTER SPLICE AT FRAME 89. MAINTENANCE R & R THE RT CENTER SPLICE AT FRAME 89 IAW SRM 51-40-02, 51-23-04, 51-21-02, 51-43-03.
DURING INSPECTION, CORROSION WAS FOUND ON THE LT GUSSET AT FRAME 90. MAINTENANCE R & R THE GUESSET PLATE IAW SRM 51-41-02.
DURING INSPECTION, CORROSION WAS FOUND ON THE RT CENTER GUSSET PLATE AT FRAME 90. MAINTENANCE R & R THE GUSSET PLATE IAW SRM 51-40-02.
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER SHEAR PLATE AT FRAMES 87-88. MAINTENANCE R & R THE SHEAR PLATE IAW SRM 51-42-02.
DURING INSPECTION, CORROSION WAS FOUND ON THE RT SHEAR PLATE AT FRAMES 87-88. MAINTENANCE R & R THE SHEAR PLATE IAW SRM 51-23-00.
DURING INSPECTION, CORROSION WAS FOUND ON THE AFT PASSENGER DOOR SILL. MAINTENANCE R & R THE AFT PASSENGER DOOR SILL IAW SRM 51-43-01.
DURING INSPECTION, CORROSION WAS FOUND ON THE AFT SERVICE DOOR SILL. MAINTENANCE R & R THE THRESHOLD IAW SRM 51-41-01, 51-41-02, 51-41-03.
DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT UPPER SHEET AT FRAMES 85-86. MAINTENANCE R & R THE UPPER SHEET AT FRAMES 85-86 IAW SRM 51-41-01, 51-43-01.
DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT DOUBLER AT FRAMES 19-20. MAINTENANCE R & R THE LT DOUBLER IAW SRM 51-41-01.
DURING INSPECTION, CORROSION WAS FOUND AT THE RT AFT FLOOR SILL AT FRAMES 17-20. MAINTENANCE R & R THE FLOOR SILL IAW SRM 51-41-02, 51-43-02.
DURING INSPECTION, A TOOL MARK WAS FOUND ON THE CENTER CROSS FRAME 17. MAINTENANCE REPAIRED THE BEAM IAW ETD2015-170-092901.
DURING INSPECTION, CORROSION WAS FOUND ON THE RT CROSS FRAME 17. MAINTENANCE REPAIRED THE CORROSION IAW ETD2015-170-092901.
DURING INPSECTION, CORROSION WAS FOUND AT THE R2 THRESHOLD AROUND THE RIVET HEADS AT THE GRIT BAR FITTING. MAINTENANCE R & R THE THRESHOLD IAW SRM 51-40-02, 51-41-01, 51-41-02, 51-43-03, 51-43-02.
MAIN CABIN DOOR DOES NOT LOCK OPEN. L1 DOOR HINGE TRIM WAS TOUCHING LATCHING HOOK MECHANISM. ADJUSTED IAW AMM 25-23-08.
FIRST EMERGENCY LIGHT STRIP INOPERATIVE. R & R THE LIGHT IAW AMM 33-50-21. OPS GOOD.
FWD PAX EXIT LOCATOR SIGNS INOPERATIVE. FOUND CONNECTOR DISCONNECTED. MATED FEMALE PLUG WITH MALE PLUG, PEFORMED OPS CHECK OF LOCATOR SIGNS, OPS CHECKED GOOD IAW JC S33-50-01-720-801A.
EMERGENCY LIGHT IN PASSENGER CABIN OUT. R & R BATTERY NR 4 IAW AMM 33-50-01. OPS GOOD.
L2 DOOR DOESN`T OPEN OR CLOSE PROPERLY. ADJUSTED AND OPS CHECKED L2 DOOR DISARMING MECHANISM IAW AMM 52-12-20.
L1 EMERGENCY OPENING PNEUMATIC ASSY BOTTLE PRESSURE IS AT 0 PSI. REPLACED L1 DOOR BOTTLE DIAPHRAGM IAW AMM 52-11-53, SERVICED IAW AMM 52-11-51.
ARMED & DISARMED INDICATOR ON L1 DOOR SHOWS ONLY PARTIAL RED OR GREEN. REPLACED L1 DOOR MAIN UPPER LINER IAW AMM 25-23-04, OPS CHECKED GOOD.
CORROSION ON FWD CARGO BAY FWD FINGER DOUBLER IN NUMEROUS AREAS. R & R FWD CARGO FWD FINGER DOUBLER.
CORROSION ON FWD CARGO AFT FINGER DOUBLER. R & R FWD CARGO AFT FINGER DOUBLER.
CORROSION ON AFT CARGO CUTOUT FLOORBOARD. R & R AFT CARGO FLOORBOARD.
CORROSION AT FLOORBEAM RT FR 87. R & R FLOORBEAM.
CORROSION ON GUSSETT PLATE LT CENTER FR91. R & R LT GUSSET.
CORROSION ON SEAT TRACK FR 84. R & R SEAT TRACK FROM FR84 TO FR80.
CORROSION ON RT SHEAR PLATE TO INCLUDE SPLICE PLATE FR87/88. R & R RT SHEAR PLATE.
CORROSION ON LT FLOOR SUPPORT FRAMES 88-90. R & R SUPPORT.
CORROSION ON TIE DOWN NUT PLATE FITTING UNDER LT SHEAR PLATE. BLENDED CORROSION, REPAIRED FITTING. MAJOR REPAIR.
CORROSION ON RT CENTER SPLICE PLATE FR90. R & R RT CENTER SPLICE PLATE.
CORROSION ON RT FLOOR SUPPORT. R & R FLOOR SUPPORT.
CORROSION ON UPPER SHEET RT FR85. R & R UPPER SHEET.
CORROSION ON CENTER SPLICE PLATE FR90. R & R CENTER SPLICE PLATE.
CORROSION ON SEAT TRACK LT FR 84, R & R CORRODED SECTION OF SEAT TRACK.
CORROSION ON UPPER SHEET LT BETWEEN FR85 AND 86. R & R UPPER SHEET.
CORROSION ON BEAM LT FR87 AND 89 AROUND SCREW HOLES. R & T BEAM FROM FR87 TO 89.
CORROSION ON CENTER SHEAR PLATE FR87/88. R & R CENTER SHEAR PLATE.
CORROSION ON RT FLOOR SUPPORT AT FR84. R & R FLOOR SUPPORT.
L1 DOOR LINER IS PREVENTING ARM/DISARM HANDLE TO ACTUATE AND INDICATING DOOR OPEN IN COCKPIT. INSPECTED AND PERFORMED ADJUSTMENT OF L1 DOOR LINERS IAW AMM 20-00-00. OPS CHECK GOOD.
"ARMED" INDICATION ON L1 DOOR IS NOT ALIGNED WITH WINDOW. RE-SECURED SCREW ON VENT FLAP COVER, "ARMED" INDICATION NORMAL, NO FUTHER DEFECTS.
R1 AFT DOOR LATCH LOCK INDICATOR NOT GREEN WITH DOOR CLOSED. RE-ATTACHED COMMAND RAMP TO R1 DOOR SHAFT IAW AMM 52-41-00-05. OPS CHECK GOOD.
L1 DOOR WOULD NOT ALLOW F/A TO RAISE DURING DISARMING HANDLE AND VENT FLAP HANDLE ALL THE WAY TO THE TOP. ADJUSTED L1 DOOR ARM/DISARM INDICATOR LINKAGE IAW AMM 52-11-00-05. OPS CHECK GOOD.
L1 DOOR SLIDE HANDLE AND VENT FLAP HANDLE DO NO ALIGN WHEN DOOR IS DISARMED. CLEANED AND LUBED DOOR HANDLE AND PERFORMED ADJUSTMENT AND TEST IAW AMM 52-12-52. OPS CHECK GOOD.
L2 DOOR SLIDE IS NOT SHOWING ARMED OR DISARMED ON SLIDE INDICATION. REPLACED BROKEN CONTROL ROD L2 DOOR INDICATION AND ADJUSTED PER AMM 52-42-00. OPS CHECK GOOD.
L1 DOOR CLOSED GREEN INDICATOR WINDOW IS NOT POSITIONED CORRECTLY ON AFT POSITION OF SURROUND. REMOVED AFT PORTION OF L1 DOOR SURROUND FOM. REPAIRED L1 SURROUND VIEWING WINDOW LOCATION IAW EMB 170 MM 25-00-19, RE-INSTALLED REPAIRED L1 DOOR SURROUND AFT PORTION IAW EMB 170 MM 25-23-08. OPS CHECK GOOD.
WINDOW THAT INDICATES GREEN ON MAIN CABIN DOOR HAS INDICATOR MISALIGNED SO THE GREEN INDICATION IS NOT SHOWING CORRECTLY. MAINTENANCE DEFERRED. ON 4/16/12 MAINTENANCE REPAIRED THE L1 DOOR SURROUND VIEW WINDOW.
R2 DOOR WILL NOT ARM. TROUBLESHOT AND FOUND AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE MECHANISM SHEARED. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY SLIDE MECHANISM IAW EMB 170 MM 52-42-40. OPS CHECK GOOD IAW AMM 52-42-4.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON WASTE SERVICE DOOR AND HINGE. MX REMOVED AND REPLACED THE HINGE AND FOUND NO DAMAGE TO THE DOOR IAW EMB 170 SRM 51-44-02. CLEANED AND RESTORED TOP COAT IAW EMB 170 CMM 25-22-40 AND SRM 51-23-06. A/C STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
CREW REPORTED THE THE L-1 DOOR SLIDE WAS BLOWN. MAINTENANCE REMOVED AND REPLACED SLIDE PER EMB AMM.
AIRCRAFT HAS A MAJOR REPAIR BEING ACCOMPLISHED. DAMAGE FOUND ON LEFT SIDE OF ACFT FUSELAGE, FRAME 9, STR 17-18L. MAINTENANCE HAS CONTACTED MANUFACTURER ENGINEERING FOR REPAIR INFORMATION. ENGINEERING HAS ISSUED EDT2010-170/10483 FOR REPAIR ACCOMPLISHMENT. REPAIR BEING ACCOMPLISHED PER THE ETD AND SRM. ACFT CURRENTLY OUT OF SERVICE FOR THE REPAIR.
GENERATED WHILE A/C WAS IN HEAVY CHECK, FR 90 GUSSET AT RT SEAT TRACK BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GUSSET AT RT SEAT TRACK BEAM IAW EMB SRM 51-41-02. A/C IS STILL CURRENTLY OUT OF SERVICE FOR HEAVY CHECK.
GENERATED WHILE A/C WAS IN HEAVY CHECK, SHEAR PLATE BETWEEN FR 87 AND FR 88 BETWEEN LT SEAT TRACK BEAM AND RT SEAT TRACK BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CENTER SEAT PLATE IAW EMB SRM 51-42-01. A/C IS STILL CURRENTLY IN HEAVY CHECK.
GENERATED WHILE A/C WAS IN HEAVY CHECK, SHEAR PLATE BETWEEN FR 87 TO FR 88, LT SEAT TRACK BEAM, AND LT CREASE BEAM HAD CORROSION. MAINTENANCE REMOVED AND REPLACED LT SHEAR PLATE IAW EMB SRM 51-41-01 AND REPAIRED TOPCOAT ON LT SEAT TRACK IAW EMB SRM 51-32-06, NO DAMAGE NOTED, ONLY TO TOPCOAT. A/C IS STILL CURRENTLY IN HEAVY CHECK.
GENERATED WHILE A/C WAS IN HEAVY CHECK, SHEAR PLATE BETWEEN FRAME 87 TO FRAME 88 AND RT SEAT TRACK BEAM AND RT CREASE BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED RT SHEAR PLATE IAW EMB SRM 51-42-01 AND REPAIRED TOPCOAT ON RT SEAT TRACK IAW EMB SRM 51-23-06, NO DAMAGE NOTED, ONLY TO TOPCOAT.
GENERATED WHILE A/C WAS IN HEAVY CHECK, SILL PLATE AT FR 89 TO RT CREASE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED RT SILL PLATE IAW EMB SRM 51-40-02, 51-42-01, AND 51-43-01. A/C IS CURRENTLY STILL IN HEAVY CHECK.
GENERATED WHILE A/C WAS IN HEAVY CHECK, SPLICE PLATE AT FR 89 LT SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED LT SPLICE PLATE IAW EMB SRM 51-43-01. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK.
GENERATED WHILE A/C WAS IN HEAVY CHECK, GUSSET AT FWD WASTE TANK SUPPORT FRAME 90 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GUSSET AT FWD WASTE TANK SUPPORT FRAME 90 IAW EMB SRM 51-41-02. A/C IS STILL CURRENTLY OUT OF SERVICE FOR HEAVY CHECK.
CREW REPORTED ALL LIGHTS IN THE CABIN WERE INOP. MAINTENANCE TROUBLESHOT AND CYCLED POWER PER EMB AMM 24-72-02, AFTER THAT ALL OF THE LIGHTS OPERATED NORMALLY.
NR 1 ENGINE FADEC WAS REMOVED DUE TO HISTORY OF FADEC FAULTS AND NO DISPATCH MESSAGE. MAINTENANCE REPLACED NR 1 ENGINE FADEC. (M)