N872RW

Part: NONE — NONE (ZONE 500) · airframe 35,805 hrs · 23,617 cycles

BLEED 1 FAIL AT 19,000 FEET. BLEED 2 USED UNDER CAPTAIN'S AUTHORITY. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. OPERATIONAL TEST OF THE AIR BLEED SYSTEM IAW AMM 36-00-00, CHECKS GOOD.

Part: FASTENER — CORRODED · airframe 34,568 hrs · 22,681 cycles

CORROSION AROUND FASTENERS AS MARKED ON STRINGER 29R FR 76-79. REPLACED RIVETS REF SRM 51-40-08. SPLICE REPAIR STRINGER 29R FR 75-82 REF ETD2022-170-002992

Part: BEAM — CORRODED · airframe 34,568 hrs · 22,681 cycles

FORWARD PASSENGER DOOR CUTOUT LOWER BEAM IS CORRODED, FR 17-18. REPLACED LOWER BEAM PN 170-03719-005 REF SRM 51-40-08. RESTORED FINISH REF SRM 51-23-04, 51-23-05, 51-23-06.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 34,568 hrs · 22,681 cycles

CORROSION ON SHEAR CLIP AT FR 86 STGR 28R-27R. REPLACED SHEAR CLIP AT FR 86 STGR 27R - 28R REF SRM 51-40-08.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 34,568 hrs · 22,681 cycles

SHEAR CLIP CORRODED AT FR 81-STGR 20R-21R. REPLACED SHEAR CLIP AT FR 81 STGR 20R-21R REF SRM 51-40-08

Part: NONE — NONE (ZONE 800) · airframe 33,964 hrs · 22,247 cycles

L1 DOOR HALF CLOSED WITH HANDLE LEVER DOWN. UNABLE TO REOPEN. RE-ALIGNED L1 DOOR TRACK AND BELL CRANK STOPS, IAW AMM 52-11-20.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,608 hrs · 22,009 cycles

EMERGENCY LIGHT POWER UNIT #6 INOP. R&R EMERGENCY LIGHT POWER UNIT #6 IAW AMM 33-50-01.

Part: ENGINE — VIBRATION (NR 2) · airframe 32,613 hrs · 21,229 cycles

ENGINE 2 LP VIBES AT 4.1. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED ENG 2 HIGH POWER RUNS, NO DEFECTS NOTED. PERFORMED VIBRATION RUNS, ALL INDICATIONS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,341 hrs · 21,006 cycles

R2 DOOR, LAST AISLE ROW AND ROW 9 EMERGENCY LIGHTS WILL NOT TURN ON, CHARGED ELPU.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 31,657 hrs · 20,473 cycles

DENT FOUND ON L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 5-6 AND BETWEEN FRONT SPAR AND STR 01 L. MAINTENANCE REPAIRED THE L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 5-6 AND BETWEEN FRONT SPAR AND STR 01 L. IAW EMB ETD 2019-170-157527.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 31,657 hrs · 20,473 cycles

DENT FOUND ON L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 3A-4 AND BETWEEN STR 01 L AND 02 L. MAINTENANCE REPAIRED THE L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 3A-4 AND BETWEEN STR 01 L AND 02 L. IAW EMB ETD 2019-170-157527.

Part: PROFILE — CRACKED (FRAME 52) · airframe 31,657 hrs · 20,473 cycles

CRACK FOUND ON CENTER FUSELAGE I WHEEL WELL FRAME PROFILE AT FR52, L/H SIDE. MAINTENANCE REMOVED AND REPLACED THE CENTER FUSELAGE I WHEEL WELL FRAME PROFILE AT FR52, L/H SIDE IAW EMB SRM 51-41-01.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 31,657 hrs · 20,473 cycles

DENT FOUND ON L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 4-5 AND BETWEEN FRONT SPAR AND STR 01 L. MAINTENANCE REPAIRED THE L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 4-5 AND BETWEEN FRONT SPAR AND STR 01 L. IAW EMB ETD 2019-170-157527.

Part: SENSOR — FAILED (LE SLAT) · airframe 28,862 hrs · 18,324 cycles

SLAT FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R LTOB 3/4 SLAT SKEW SENSOR IAW AMM 27-83-01. R&R W512 WING SLAT 3/4 LT HARNESS IAW AMM 27-83-07. R&R RTOB 3/4 SLAT SKEW SENSOR IAW AMM 27-83-01. R&R W612 WING SLAT 3/4 RT HARNESS IAW AMM 27-83-07. PERFORMED SLAT RIGGING AND OPS CHECK IAW AMM 27-80-00.

Part: LEVER — LACK OF LUBE (R1 DOOR) · airframe 28,156 hrs · 17,839 cycles

R1 DOOR ARMING LEVER WAS STICKING. LUBRICATED THE DOOR ARMING LINKAGE IAW AMM 52-11-00.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE THE ACFT IS IN HEAVY CHECK FOUND CORROSION AT AFT WET AREA AT FR 90 RT SIDE OF SPLICE. REMOVED AND INSTALLED NEW SHAPE SPLICE AT AFT WET AREA FR 90 RT SIDE, REF SRM 51-40-08. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE ACFT IS IN HEAVY CHECK FOUND CORROSION ON LT FLOOR SILL AT FR 87-90 IN FRONT OF WASTE TANK. REMOVED AND INSTALLED NEW FLOOR SILL AT FR 87-90 IN FRONT OF WASTE TANK. REF SRM 51-40-08. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE ACFT IS IN HEAVY CHECK FOUND CORROSION AT AFT WET AREA FR 90 CENTER SPLICE FITTING. REMOVED AND INSTALLED NEW INTERCOSTAL AND NEW SPLICE AT FR 90. REF SRM 51-40-08. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE ACFT IS IN HEAVY CHECK FOUND CORROSION. AFT WET AREA CENTER CROSS BEAM AT FR 90. REMOVED AND REPLACED CENTER CROSS BEAM AREA FR 90 REF SRM 51-40-08, 51-40-02 AND 51-23-04. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE ACFT IS IN HEAVY CHECK FOUND CORROSION. PASSENGER CABIN RT HAND O/B SEAT TRACK FR 74 - 85. REMOVED AND REPLACED PASSENGER CABIN RT HAND O/B SEAT TRACK FR 74-85 REF SRM 51-40-08, 51-23-06. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE ACFT IN HEAVY CHECK FOUND CORROSION ON FRAME 87 LONGITUDINAL BEAM RIGHT SIDE. REMOVED AND INSTALLED NEW RT LONGITUDINAL BEAM AT FR 85/88 REF SRM 51-40-08E.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE IN HEAVY CHECK CORROSION FOUND AT AFT WET AREA FRAME 90 ON THE RIGHT SIDE FLOOR SILL. REMOVED AND INSTALLED NEW RIGHT SIDE FLOOR SILL AT FRAME 90 REF SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE IN HEAVY CHECK CORROSION FOUND AT FRAME 87-88 SPLICE PLATE ON THE LEFT SIDE. REMOVED AND INSTALLED NEW LEFT SHEAR PANEL AND SPLICE REF SRM 51-40-02, 51-23-04, AND 51-40-08.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

WHILE IN HEAVY CHECK FOUND CORROSION AT FR 89 LT. SIDE OF THE LONGITUDINAL BEAM. REMOVE AND REPLACE BEAM WITH NEW REF SRM 51-23-04 AND 51-41-01.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION AFT LOWER FUSELAGE FR 88 BETWEEN STR 28-27 HAS CORRODED SHEAR CLIP AS MARKED. (MAJOR FCS) REMOVED AND REPLACED CORRODED SHEAR CLIP AFT LOWER FUSELAGE FR 88 BETWEEN STR.28R-27R DRILLED NEW SHEAR CLIP AND ALODINE REF SRM 51-40-08, 51-40-02 AND 51-23-04.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION AFT LOWER FUSELAGE FR 87 BETWEEN STR 28-27 HAS CORRODED SHEAR CLIP AS MARKED. REMOVED AND REPLACED CORRODED SHEAR CLIP AFT LOWER FUSELAGE FR 87 BETWEEN STR 28R-27R. DRILLED NEW SHEAR CLIP AND ALODINE REF SRM 51-40-08, 51-40-02 AND 51-23-04.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION AFT LOWER FUSELAGE FR.86 - FR.87 BETWEEN STR 28-27 HAS CORRODED BRACKET AS MARKED. REMOVED AND REPLACED CORRODED BRACKET AFT LOWER FUSELAGE FR86 - FR87 BETWEEN STR 28R-27R. DRILLED NEW BRACKET AND APPLIED ALODINE REF SRM 51-40-02,51-40-08 AND 51-23-04.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND RIGHT HAND HORIZONTAL STABILIZER RIB 11 AT FRONT AND MIDDLE SPAR HAS A CRACK. REMOVED DAMAGED RIB 11 FROM RT HORIZONTAL STAB. LOCATED, DRILLED, ALODINED AND INSTALLED NEW RIB 11 ON RT HORIZONTAL STAB REF SRM 51-40-08, 51-41-01, 51-41-02.

Part: SKIN — GOUGED (LT HORIZ STAB) · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND LEFT HAND UPPER HORIZONTAL SKIN HAS GOUGE AT RIB 6. (MAJOR REPAIR) REPAIRED GOUGE BY INSTALLING INTERNAL REPAIR DOUBLER REF ETD2018-170-022426.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND PASSENGER CABIN LT HAND O/B SEAT TRACK FR 23-34, HAS CORROSION AT FR 24, GOUGED AT FR 25, CORROSION AT FR 26, GOUGED AT FR 27, CORROSION AT FR. 28, GOUGED AT FR 30. REMOVE AND REPLACE SEAT TRACK WITH NEW P/N 170-67373-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CHAFED/CORROSION ALONG PASSENGER CABIN RT I/B SEAT TRACK 23 - 34. REMOVED AND REPLACED PASSENGER CABIN RT I/B SEAT TRACK FRAME 23-34 REF SRM 51-40-08 PN 170-67861-005.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND RIGHT HAND HORIZONTAL STABILIZER RIB 12 AT FRONT AND MIDDLE SPAR CRACKED. REMOVED DAMAGED RIB 12 AT RT HORIZONTAL STAB. LOCATED, DRILLED, ALODINED AND INSTALLED NEW RIB 12 AT RT HORIZONTAL STAB REF SRM 51-40-08, 51-41-01, 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND PASSENGER CABIN RT HAND I/B SEAT TRACK FR 74-85 HAS CORROSION AT FR 83. REMOVED AND REPLACED SEAT TRACK WITH NEW FR 74-85 P/N 170-86082-005.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION FOUND ON AFT PAX DOOR {L2} THRESHOLD LOWER BEAM ON UPPER SURFACE WEB, AND IN BOTH GIRT FITTING CUTOUT RADIUS DURING ACCOMPLISHMENT OF 170EO-53-14-0003. REMOVE AND REPLACE THRESHOLD WITH NEW P/N 170-65703-005.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND SPLICE PLATE AT THE FLOORBEAMS AT FRAME 87-88 TOP AND CENTER HAS AREAS OF CORROSION ON THE RIGHT SIDE AS MARKED. REMOVED SPLICE PLATE AT THE FLOORBEAMS AT FRAME 87-88 TOP AND CENTER REF SRM 51-40-08 DRILLED NEW PART AND APPLIED ALODINE REF SRM 51-40-02 AND 51-23-04, INSTALLED NEW CENTER SHEAR PANEL SRM 51-40-08.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION BOTH LOWER ANGLES ON PANEL 1441FR. REMOVED AND REPLACED BOTH LOWER ANGLES ON PNL 1441FR REF SRM 51-45-00.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,741 hrs · 17,577 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION BOTH LOWER ANGLES ON PANEL 1431DL. REMOVED AND REPLACED BOTH LOWER ANGLES ON PNL 1431DL REF SRM 51-45-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,442 hrs · 16,062 cycles

MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT STRIP WAS DULL AND DID NOT LIGHT UP. REMOVED AND REPLACED THE LIGHT IAW AMM AND OPS CHECKED GOOD.

Part: MECHANISM — DIRTY (R1 DOOR) · airframe 25,172 hrs · 15,891 cycles

FA REPORTS R1 ARMING HANDLE IS DIFFICULT TO OPERATE. CLEANED AND LUBED R1 ARMING HANDLE MECHANISM IAW AMM 52-11-22. OPS CHECK GOOD.

Part: LEVER — DIRTY (R1 DOOR) · airframe 25,023 hrs · 15,797 cycles

ARMING LEVER ON R1 DOOR STIFF. CLEANED AND OPS CHECKED ACTUATING UNITS ON R1 DOOR IAW AMM 52-41-01, NO DEFECTS NOTED.

Part: LIGHT — CONTAMINATED (CABIN) · airframe 24,960 hrs · 15,743 cycles

LIQUID INSIDE FWD ENTRY WAY FLOOR LIGHT STRIP. REMOVED LIGHT AT FWD ENTRY WAY FLOOR, CLEANED AND REINSTALLED IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: ROD — DAMAGED (TE FLAPS) · airframe 24,652 hrs · 15,580 cycles

FLAP FAIL, STUCK AT ZERO. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R 2 RT FLAP RODS.

Part: BRACKET — LOOSE (DOOR INDICATOR) · airframe 24,144 hrs · 15,201 cycles

R2 DOOR INDICATOR FALLING OUT OF VIEW. ALIGNED THE VIEW WINDOW BRACKET ASSY IAW AMM 52-42-22. OPS CHECK GOOD.

Part: LEVER — LACK OF LUBE (SERVICE DOOR ARM) · airframe 23,668 hrs · 14,877 cycles

FWD SERVICE DOOR ARMING LEVER STICKING, DIFFICULT TO MOVE. LUBRICATED DOOR MECHANISM FOR ARM/DISARM LEVER REF 52-41-00. OPS CHECK GOOD AFTER APPLYING A LITTLE EFFORT.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 23,624 hrs · 14,851 cycles

R1 DOOR ARMING HANDLE IS HARD TO OPERATE. TAKES A LOT OF FORCE TO MOVE WHEN ARMING AND DISARMING. FOUND BUSTLE CABLE HITTING GIRT BAR. RESECURED BUSTLE IAW AMM 25-65-01. OPS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (DOOR ARMING) · airframe 23,620 hrs · 14,849 cycles

R1 DOOR ARMING LEVER HANDLE IS DIFFICULT TO ENGAGE. LUBRICATED THE R1 DOOR ARMING ASSY IAW AMM 52-41-00. ARMING LEVER ENGAGES WITH NO ISSUES.

Part: HANDLE — LACK OF LUBE (R1 DOOR ARMING) · airframe 23,594 hrs · 14,836 cycles

R1 DOOR ARM/DISARM HARD TO OPERATE. CLEANED AND LUBED R1 DOOR AS REQUIRED, OPS CHECK GOOD IAW 52-41-00/500.

Part: LEVER — LACK OF LUBE (R1 DOOR ARMING) · airframe 23,503 hrs · 14,789 cycles

R1 DOOR ARMING LEVER DIFFICULT TO MOVE. CLEANED AND LUBRICATED R1 DOOR ARMING LEVER MECHANISM IAW CMM 52-41-22. HANDLE OPS CHECK GOOD.

Part: GIRT BAR — BINDING (R1 DOOR SLIDE) · airframe 23,489 hrs · 14,777 cycles

R1 SLIDE ARM HANDLE STIFF TO ARM. CLEANED DEBRIS FROM GIRT BAR LOCK IN FLOOR, OPS CHECK GOOD IAW MM 52-41-20.

Part: COVER — UNSECURE (R1 DOOR) · airframe 23,487 hrs · 14,776 cycles

R1 DOOR EMERGENCY SLIDE HANDLE IS STIFF TO ARM. FOUND R1 DOOR TRIM COVER HINDERING ARM HANDLE. ADJUSTED AND ATTACHED TRIM COVER AND CHECKS GOOD NOW IAW AMM 52-11-00.

Part: INDICATOR — OUT OF ADJUST (R1 DOOR) · airframe 23,443 hrs · 14,743 cycles

R1 DOOR LATCH VISUAL INDICATOR ALONG RT SIDE OF DOOR EDGE NOT SHOWING GREEN WHEN DOOR IS LATCHED AND ARMED. ADJUSTED UPPER RT INDICATOR IAW AMM 52-41-00. OPS CHECK GOOD.

Part: LEVER — OUT OF ADJUST (R1 DOOR) · airframe 23,351 hrs · 14,658 cycles

DOOR R1 ARMING LEVER VERY DIFFICULT TO MOVE. ADJUSTED R1 DOOR LEVEL IAW AMM 52-41-00.

Part: SEAL REST — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 23,345 hrs · 14,652 cycles

CORROSION ON THE AFT CARGO LOWER SEAL REST. R & R AFT CARGO LOWER CENTER SEAL REST.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,345 hrs · 14,652 cycles

RIGHT SHEAR PLATE IS CORRODED AT FRAMES 87-88. R & R RT SHEAR PLATE.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 23,345 hrs · 14,652 cycles

RIGHT CENTER GUSSET PLATE IS CORRODED AT FRAME 90. R & R RT CENTER GUSSET PLATE.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,345 hrs · 14,652 cycles

CENTER SHEAR PLATE IS CORRODED AT FRAME 87-88. R & R CENTER SHEAR PLATE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 23,334 hrs · 14,642 cycles

EMERGENCY LIGHT STRIP NOT EXPOSED AT SEAT 15C. ADJUSTED THE EMERGENCY LIGHT STRIP RT SIDE IAW AMM 33-50-21.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,257 hrs · 14,582 cycles

L2 DOOR EXIT MARKER AND EMERGENCY LIGHT WILL NOT ILLUMINATE. R & R NR 3 EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,782 hrs · 14,225 cycles

PHOTOLUMINESCENT STRIPS, ROW 1-3, RT OF A/C. R & R PHOTOLUMINESCENT STRIPS IAW AMM 33-50-21.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 22,460 hrs · 13,977 cycles

FWD AFT SERVICE DOOR EMERGENCY EXIT COVER CRACKED. R & R FWD AFT SERVICE DOOR EMERGENCY EXIT COVERS IAW AMM 33-50-17. OPS CHECKED GOOD.

Part: GLOWSTRIP — NOT REPORTED (CABIN) · airframe 22,460 hrs · 13,977 cycles

FIRST TWO RT GLOW STRIPS NEED TO BE REPLACED. R & R THE GLOWSTRIPS IAW AMM 33-50-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,263 hrs · 13,844 cycles

ILLUMINATION STRIPS 1, 2, 3 PARTIALLY ILLUMINATED. R & R ILLUMINATION STRIPS IAW AMM 33-50-21. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 21,668 hrs · 13,488 cycles

LANDING GEAR WOULD NOT RETRACT. FOLLOWED QRH, DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R & R NOSE GEAR LT PROXIMITY SWITCH IAW 32-62-01. OPS CHECK GOOD. LAST SCHEDULED SERVICING WAS 9/25/2014, WITH AN UNSCHEDULED SERVICING ON 10/25/2014.

Part: LIGHT — UNSECURE (CABIN) · airframe 20,755 hrs · 12,958 cycles

FLOOR TRIM AT 1C NOT ATTACHED. SECURED THE LIGHT STRIP AT SEAT 1C IAW MM 33-50-21.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 20,530 hrs · 12,785 cycles

EXIT MARKER LENS ABOVE R1 DOOR IS CRACKED. R & R THE LENS IAW AMM 33-50-17.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,940 hrs · 13,078 cycles

CORROSION FOUND ON MID EBAY PLUG EXTERNAL SKIN UPPER FLAGE AT NUTPLATES. REMOVED DAMAGE.

Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,940 hrs · 13,078 cycles

CORROSION FOUND ON SHEAR TIE IN AFT CARGO BAY, FRAME 84 STRINGER 28L. R & R SHEAR CLIP, MAJOR REPAIR.

Part: LIGHT — UNSECURE (CABIN) · airframe 20,172 hrs · 12,497 cycles

LARGE GAP IN CABIN FLOOR EMERGENCY LIGHT STRIP. R & R EMERGENCY LIGHT STRIP IAW AMM 33-50-21.

Part: SEAT TRACK — CORRODED (FRAME 74) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION ON LT INBD SEAT TRACK APPROXIMATELY FRAME 74. R & R SEAT TRACK.

Part: FRAME — CORRODED (84) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON FRAME 84. INSTALLED ANGLE DOUBLER IAW ETD 2014-170-057558. MAJOR REPAIR.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON RT SHEAR PLATE TO FUSELAGE FRAME 87-88. R & R RT SHEAR PLATE TO FUSELAGE SPLICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 87) · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON FWD RT FLOOR SUPPORT AT FRAME 87. R & R RT FLOOR SUPPORT.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON FWD CARGO DOOR SURROUND STRUCTURE. REPAIRED OF FWD CARGO DOOR SURROUND STRUCTURE IAW ETD 2014-170-057556, REV 1.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON L2 DOOR THRESHOLD AROUND 4 RIVETS AROUND EMERGENCY EVAC SLIDE FITTINGS. REMOVED DAMAGE IAW ETD 2014-170-057549.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON RT AFT FLOOR SUPPORT FRAMES 17-20. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON RT FWD FLOOR SUPPORT FRAMES 12 - 14. R & R FLOOR SUPPORT.

Part: THRESHOLD — CORRODED (R2 DOOR) · corrosion level 2 · airframe 20,122 hrs · 12,462 cycles

CORROSION FOUND ON R2 DOOR THRESHOLD FWD FITTING. REPAIRED THRESHOLD.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 19,967 hrs · 12,372 cycles

INDICATION ON MFD, R2 DOOR SHOWS DOOR ARMED WHEN DOOR IS NOT ARMED. INDICATION ON DOOR SHOWS DISARMED. COMPLETED OPS CHECK OF R2 DOOR LOCKING INDICATION AND SLIDE ARM/DISARM INDICATION IAW AMM 52-42-00. NO DEFECTS NOTED.

Part: LIGHT — UNSECURE (ZONE 100) · airframe 19,156 hrs · 11,868 cycles

EMERGENCY LIGHTSTRIP BY FWD GALLEY CLOSET CAME OFF OF THE FLOOR. SECURED FWD GALLEY LIGHT STRIP IAW AMM 33-51-21.

Part: LENS — LOOSE (CABIN LIGHTS) · airframe 18,309 hrs · 11,345 cycles

PIECE OF FLUORESCENT FLOOR LIGHTING NEEDS TO BE REATTACHED IN FRONT OF FWD CLOSET. RESECURED FLUORESCENT STRIP AS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,941 hrs · 11,042 cycles

EMERGENCY LIGHTING AT FWD RIGHT CABIN NOT GLOWING GREEN. REPLACED FWD EMERGENCY LIGHT IAW AMM 33-50-21.

Part: UNKNOWN — MALFUNCTIONED (L2 DOOR) · airframe 16,789 hrs · 10,224 cycles

UPON DESCENT AT 10,000 FT GOT EICAS MESSAGE L2 PAX AFT DOOR OPEN. F/A'S REPORTED DOOR INDICATION LOOKED "IN BETWEEN". PERFORMED OPS CHECK OF L2 DOOR LOCKING/SENSING IAW AMM 52-12-00. UNABLE TO DUPLICATE FAULTS, NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (L1) · airframe 16,173 hrs · 9,841 cycles

FLIGHT ATTENDANT UNABLE TO GET MAIN CABIN DOOR TO CLOSE. LUBED L1 DOOR IAW AMM 52-11-22, OPS CHECK GOOD IAW AMM 52-11-20.

Part: SPAR — CRACKED (RT WING) · airframe 15,727 hrs · 9,512 cycles

MAJOR REPAIR - PERFORMED HFEC ON SPAR II RIGHT WING IAW EMB TASK CARD S170EO-57-10-0003, STEP 22, FOUND CRACK LIKE INDICATION IN HOLE A2, CRACK FACING AFT IN HOLE, UP 1/4" GREATER THAN .30. DRILLED AND REAMED HOLE TO 0.359 IAW SRM 51-40-02. PERFORMED HFEC ON SPAR II RIGHT WING IAW TASK CARD, NO CRACK LIKE INDICATIONS FOUND AT THIS TIME, 0.365 IS ACCEPTABLE IAW ETD 2012-170-011490.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 15,727 hrs · 9,512 cycles

MAJOR REPAIR - FORWARD CARGO DOOR LOWER CENTER SEAL REST CORRODED, LEVEL 2. REMOVED AND REPLACED LOWER FWD CARGO SEAL REST CENTER IAW EMB 170 SRM 51-40-02, 51-41-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,571 hrs · 9,421 cycles

L2 DOOR OVERHEAD EMERGENCY DOOR LIGHT INOP. REMOVED AND REPLACED AFT I/B EMERGENCY LIGHT BATTERY IAW EMB 170 AMM 33-50-01, OPS CHECK GOOD.

Part: SCREW — DEFECTIVE (R1 DOOR) · airframe 15,571 hrs · 9,421 cycles

R1 DOOR BUSTLE FWD FASTENER WILL NOT ENGAGE. REMOVED AND REPLACED R1 DOOR BUSTLE SCREWS AND INSTALLED IAW EMB 170 MM 25-23-0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,571 hrs · 9,421 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R1 DOOR EMERGENCY LIGHT IAW EMB 170 MM 33-50-0.

Part: DOOR — LACK OF LUBE (L1) · airframe 14,567 hrs · 8,836 cycles

F/A REPORTS L1 DOOR HANDLE DIFFICULT TO OPEN. LUBED AND OPS CHECK L1 DOOR IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: DOOR — OBSTRUCTED (L1) · airframe 13,773 hrs · 8,404 cycles

COULD NOT DISARM L1 DOOR. REMOVED DEBRIS FROM LOWER DOOR FRAME, PERFORMED ARMED/DISARMED CHECK. OPS CHECK GOOD IAW EMB 170 MM 52-11-00.

Part: INDICATOR — INTERMITTENT (L1 DOOR) · airframe 13,583 hrs · 8,285 cycles

L1 VISUAL DOOR LOCK INDICATOR INTERMITTENT. REMOVED AND REPLACED L1 DOOR VISUAL LOCK INDICATOR IAW EMB 170 MM 52-11-22. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,028 hrs · 7,944 cycles

CREW REPORTED HEAVY OIL SMELL ON CLIMBOUT, SMELL SUBSIDED AFTER CLOSING BLEED NR 1. MAINTENANCE DEFERRED BLEED NR 1. AUG 9 - C/W 170EI-75-20-0012 JOBCARD - BOROSCOPE NR 1 ENG COMPRESSOR SECTION, NO OIL EVIDENCE FOUND IN COMPRESSOR. INSPECTED A SUMP, NO LEAKS NOTED. REF MM 72-00-00 INSP 002.

Part: INDICATOR — OUT OF ADJUST (R1 DOOR) · airframe 12,910 hrs · 7,877 cycles

R1 DOOR LATCH INDICATOR NOT SHOWING GREEN. ADJUSTED AFT WALL MECHANICAL INDICATOR ON R1 DOOR, OPS CHECK GOOD IAW EMB 170 MM 52-11-00.

Part: UNKNOWN — MALFUNCTIONED (R1 DOOR) · airframe 12,200 hrs · 7,381 cycles

CREW REPORTED R-1 DOOR WAS HARD TO DISARM. MAINTENANCE PERFORMED OPERATIONAL CHECK OR R1 DOOR PER EMB AMM, NO DEFECTS WERE FOUND.

Part: SENSOR — MALFUNCTIONED (LE SLAT) · airframe 11,633 hrs · 6,985 cycles

CREW REPORTED ON APPROACH THEY RECEIVED A SLAT FAIL. CREW DECLARED AN EMERGENCY, BUT DID NOT PREPARE CABIN. AC LANDED UNEVENTFULLY AND TAXIED UNDER OWN POWER TO GATE. MX REMOVED AND REPLACED RT 2/3 AND 3/4 SLAT SKEW SENSORS PER EMB AMM, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 11,469 hrs · 6,865 cycles

CREW REPORTED EMERGENCY LIGHT AT FRONT ENTRY WAY OVER CENTER AISLE WAS INOP. MAINTENANCE RE-SECURED CONNECTOR ABOVE AND FORWARD OF THE LIGHT PER EMB AMM.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON THE AFT OUTBOARD FLOOR MOUNT IN THE FORWARD GALLEY. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE AFT OUTBOARD FLOOR MOUNT IN THE FORWARD GALLEY IAW EMB 170 AMM 20-10-01 & 25-31-01.

Part: BRACKET — CORRODED (WASTE BOX) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE BONDING BRACKETS ON INTERNAL SIDE OF WASTE DRAIN BOX. MX REPLACED WASTE BOX P/N 170-85084-405 IAW EMB 170 SRM 51-43-02. A/C REMAINS IN CMH FOR CHECK COMPLETION.

Part: PIN — CORRODED (LT MLG ACTUATOR) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE LT MLG ACTUATOR PIN. MX REPLACED THE RT MLG ACTUATOR PIN P/N 1840-0006 IAW EMB 170 AMM 32-31-31. A/C REMAINS IN CMH FOR CHECK COMPLETION.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE FLOOR CROSSBEAM AT FRAME 17 BETWEEN LT AND RT LONGITUDINAL BEAMS. MAINTENANCE REMOVED AND REPLACED THE FLOOR CROSSBEAM AT FRAME 17 IAW EMB 170 SRM 51-40-02, 51-41-02, 51-43-02 & 51-43-01. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON NUT PLATE BRACKET ON RT SIDE OF FR 86 CROSSBEAM. MX REPLACED THE NUT PLATE BRACKET IAW EMB 170 SRM 51-41-01. P/N 120-66796-001

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE RT SHEAR WEB AT FR 14. MX REPLACED THE SHEAR WEB P/N 170-05663.003 DRILLED IAW EMB 170 SRM 51-40-02 AND 51-40-04 AND 51-43-03 51-41-02. A/C REMAINS IN CMH FOR COMPLETION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FLOORBEAM O/B OF RIGHT LONG BEAM AT FRAME 14. MAINTENANCE REMOVED AND REPLACED FLOORBEAM AT FRAME 14 IAW EMB 170 SRM 51-41-02, 51-43-01, 51-40-02 & 51-41-01. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON FR 17-18 LT LONGITUDINAL BEAM. MX REPLACED LT SEAT TRACK IAW EMB 170 SRM 51-41-01, 51-43-01, P/N 170-03264-001. A/C REMAINS IN CMH FOR COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE RT FLOOR SUPPORT BETWEEN FR 88-90. MX REPLACED RT FLOOR PANEL SUPPORT P/N 170-86181-005 IAW EMB 170 SRM 51-42-01 AND 51-43-01. A/C REMAINS IN CMH FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON RT LONG BEAM FROM FR14-18. MX REPLACED THE RT SEAT TRACK BEAM P/N 170-03263-001. FROM FR 12 TO FR 20 IAW EMB 170 SRM 51-40-02. A/C REMAINS IN CMH FOR COMPLETION.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE SPLICE AT THE LT SHEAR PANEL AT FR 87-88. MX REPLACED THE LT SHEAR PLATE IAW EMB 175 SRM 51-42-01. P/N 170-65644-001 A/C REMAINS IN CMH FOR COMPLETION.

Part: RIVET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON RT LONGITUDINAL BEAM AT FR 86 INTERSECTION. MX FOUND CORROSION TO BE ON RIVET HEADS ONLY. REPLACED RIVETS IAW EMB 170SRM 51-41-01. AC REMAINS IN CMH FOR COMPLETION. P/N MS20470AD-5-5.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE CENTER SHEAR WEB AT FR 87-88. MX REPLACED THE CENTER SHEAR WEB IAW EMB 175 SRM 51-42-01. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON THE RT SHEAR WEB AT FR 87-88, MAINTENANCE REMOVED AND REPLACED RT SHEAR PANEL WEB AT FR 87-88 IAW EMB 170 SRM 51-42-01. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,227 hrs · 6,689 cycles

WHILE A/C WAS IN HEAVY CHECK FOUND LEVEL 2 CORROSION ON THE LT SHEAR PANEL AT FR 87 AND FR 88. MX REPLACED THE LT SHEAR PANEL IAW EMB 175 SRM 51-42-02. A/C REMAINS IN CMH FOR COMPLETION. P/N 170-65927-007.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 10,772 hrs · 6,335 cycles

CREW REPORTED HOT BRAKES ON LANDING, AND DECLARED AN EMERGENCY. A/C CAME TO GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF BRAKES PER EMB AMM, AND NO DEFECTS WERE FOUND. A/C WAS RETURNED TO SERVICE.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 10,045 hrs · 5,864 cycles

CREW REPORTED L-1 DOOR SLIDE UNLACED. MAINTENANCE REMOVED AND REPLACED L-1 DOOR EMERGENCY EVACUATION SLIDE PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.

Part: HANDLE — MALFUNCTIONED (R1 DOOR) · airframe 9,781 hrs · 5,680 cycles

CREW REPORTED R-1 DOOR HANDLE WAS HARD TO USE. MAINTENANCE PERFORMED OPS CHECK OF R-1 DOOR PER EMB AMM, NO FAULTS FOUND AND A/C WAS RETURNED TO SERVICE.

Part: LEVER — LACK OF LUBE (R1 DOOR) · airframe 9,607 hrs · 5,572 cycles

CREW REPORTED R-1 DOOR ARMING LEVER WAS HARD TO ENGAGE AND DISENGAGE. MAINTENANCE LUBED R-1 DOOR PER EMB AMM, OPS CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (SPOILER SYS) · airframe 9,256 hrs · 5,379 cycles

CREW REPORTED, RECEIVED A SPOILER FAULT AFTER DEPARTING MCI, CREW COULDN'T CLEAR MSG AFTER FOLLOWING QRH. THE CREW DECIDED TO CONTINUE AND DECLARED AN EMERGENCY INTO LGA AND LANDED WITHOUT INCIDENT. MTX WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT, AND REST THE FCM 1 AND PERFORMED FLIGHT CTRL RTS PER EMB AMM AND THE MSG CLEARED. A/C WAS THEN RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (NR 2) · airframe 6,518 hrs · 3,846 cycles

ON FINAL APPROACH TO MCI, EICAS INDICATION MESSAGE HYD QTY 2 LOW. CREW CHECKED QTY SAW IT WAS ERRATIC BUT STABLE. CREW OPTED TO GO AROUND AND RUN THE CHECKLIST. THE CHECKLIST STATED ITS JUST AN ADVISORY MESSAGE, ALSO RAN THROUGH THE NO FLUID QUANTITY JUST AS A PRECAUTION TO BECOME FAMILIAR WITH IT IN CASE SYSTEM WAS COMPLETELY LOST. LANDED FLAPS FULL AND ONCE THE REVERSE AND SPOILERS DEPLOYED STEERING BECAME REALLY SLUGGISH BUT STILL WORKED. DISCREPANCY WROTE UP, MAINT WAS DISPATCHED AND SERVICED NR 2 HYD SYSTEM PER EMB AMM. AC RELEASED FOR FLIGHT.

Part: SENSOR — BROKEN (LE SLAT) · airframe 6,243 hrs · 3,689 cycles

CREW REPORTED SLAT FAIL ON APPROACH TO MKE AND DIVERTED TO ORD. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. ORD MAINT CALLED TO AC, PERFORMED AC DOWNLOADS. MAINT FOUND LEFT O/B SLAT SKEW SENSOR 3/4 BROKE IN HALF. MAINT REPLACED SKEW SENSOR PER EMB AMM. OPERATION CHECKS GOOD. RETURNED AC TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 1,304 hrs · 706 cycles

FLIGHT 6503 LGA TO DCA BURNT SMELL IN COCKPIT AFTER ENGINE SHUTDOWN. OCM VERIFIED NO C/B'S TRIPPED, NO SMELL WITH POWER ON, PERFORMED VISUAL IN FWD AVNX BAY, NO DEFECTS NOTED. OCM RAN ENGINES AND NO SMELL NOTED. NO REPEAT DISCREPANCIES TO THIS DATE 03/05/2007.