N646AE

Part: FLASHLIGHT ASSY — INOPERATIVE (ZONE 200) · airframe 52,262 hrs · 49,344 cycles

AFT EMERGENCY FLASHLIGHT INOP. RAR FLASHLIGHT ASSY IAW AMM33-50-16

Part: SKIN — CRACKED (ZONE 300) · airframe 52,025 hrs · 49,059 cycles

FUSELAGE UPPER SKIN PLATE, JUST FWD OF RUDDER 1, AT FR 81 CRACKED INSIDE 312AR. R&R CRACKED FUSELAGE UPPER SKIN PLATE, JUST FWD OF RUDDER 1, AT FR81 INSIDE 312AR IAW EMB145 SRM 51-40-02 AND SRM 51-20-01.

Part: SKIN — DAMAGED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

DMT 17 PERMANENT REPAIR OF LIGHTENING STRIKE DAMAGE PER EMB SRM 53-22-01 ETD2023-145-008587. FRAM 26-FRAM 27, STGR 20L- STGR 21.C/W PERMANENT REPAIR IAW EMB 145 SRM 53-22-01 REF ITEM 2, FIG 201, SHEET 1, REPAIR TYPE "A".

Part: REPAIR — INCORRECT (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

FRAME 12A REPAIR STGR 16L PREVIOUS REPAIR DOUBLER HAS NO DTI INFORMATION. INSTALLED DOUBLER AND FILLER ON FUSELAGE SKIN AT FR12A STGR 16L IAW ETD2025-145-927153 REV B AND PIEDMONT EO1-53-25-0305.

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

FUSELAGE CERVICE DOOR CUT-OUT AT FR-22 AND BETWEEN STGR 15R-16R HAS CORROSION. REPAIRED IAW 145 SRM 53-00-04RE, ITEM 16 FIG 208 AND PIEDMONT EO 53-25-0297.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

CENTER AMEGA BEAM GUSSET PITTED IN NUMEROUS AREAS BETWEEN FR. 23-28. R&R CENTER OMEGA BEAM GUSSET BETWEEN FRAMS 23-28 IAW EMB 145 SRM 51-40-02.

Part: FRAME — CHAFED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

FR 9 IS CHAFED BETWEEN STGR 9L-10L JUST BELOW PILOTS DV WINDOW. R & R FR 9 BETWEEN STGR 9L-10L JUST BELOW PILOTS DV WINDOW IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,025 hrs · 49,059 cycles

LH OMEGA BEAM CENTER ISLE FLOOR SUPPORT FLANGE CORRODED IN NUMEROUS SREAS ALONG ENTIRE LENGHT BETWEEN FR 23-36 INCLUDING PREVIOUSLY BLENDED AREA. BLENDED AREA ACCEPTED AS IS IAW ETD2025-145-925994.

Part: SKIN — CRACKED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

LH REAR FUSELAGE 2 UPPER SKIN RIVET ON FR80 BETWEEN STR 6L-7L HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON LH REAR FUSELAGE 2 UPPER SKIN AT FR80 BETWEEN STGR 6L-7L IAW EMB 145 SRM 53-32-01 REF STEP 9 AND PIEDMONT EO1-53-25-0291.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH OMEGA BEAM GUSSET HAS PITTING IN NUMEROUS AREAS ALONG ENTIRE LENGTH BTWN FR 23-36. R&R LH OMEGA BEAM GUSSET BETWEEN FR23-36 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

L/H LOWER SEAT TRACK #3 HAS CORROSION IN MULTIPLE AREAS. R&R L/H SEAT TRACK #3 IAW EMB 145 SRM 53-00-11AD AND AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

CENTER OMGA BEAM SUPPORT IS CORRODED BETWEEN FR. 52-53. R&R CENTER OMGA BEAM FLLOR SUPPORT BETWEEN FR. 52-53 IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

LAV L/H POTABLE WATER CABLE SUPPORT IS CORRODED. R&R LAV L/H POTABLE WATER CABLE SUPPORT IAW EMB 145 SRM 51-40-02.

Part: DOUBLER — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

GALLEY AFT DIAMOND GUSSET AT FR22 CORRODED. R & R GALLEY AFT DIAMOND GUSSET AT FR22 IAW EMB 145 SRM 51-40-02.

Part: FRAME — GOUGED (ZONE 200) · corrosion level 3 · airframe 52,025 hrs · 49,059 cycles

FRAME 65 HAS GOUGESAROUND MULTIPLE NUT PLATE HOLES, LOCATED BETWEEN STGR 2R AND 8R.C/W PERMANAENT REPAIR ON FRM65 BETWEEN STGR 2R AND 8R PER ETD2025-145-925993.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

RH CENTER SEAT TRACK #2 HAS GOUGES AND CORROSION IN NUMEROUS AREAS ALONG ENTIRE LENGHT. R&R RH CENTER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

GALLEY FLOOR CROSSBEAM AT FR18 BETWEEN LH FLOOR SILL #1 AND LH OMEGA BEAM HAS CORROSION. R&R GALLEY FLOOR CROSSBEAM AT FR18 BETWEEN LH FLOOR SILL #1 AND LH OMEGA BEAM IAW EMB 145 SRM51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

RH CENTER SEAT TRACK #2 HAS GOUGES AND CORROSION IN NUMEROUS AREAS ALONG ENTIRE LENGTH. R&R R/H CENTER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06.

Part: BUSHING — CORRODED (ZONE 300) · airframe 52,025 hrs · 49,059 cycles

HORIZONTAL STAB RH HINGE FITTING OUTBD BUSHING HOUSING #4 CORRODED.REPAIRD CORROSION IAW EMB 145 SRM 55-10-02 SEE NRTC # F061480 FOR #4 BUSHING INSTALLATION.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH REAR FUSELAGE 2 UPPER SKIN RIVET ON FR77, STGR 6L HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON LH REAR FUSELAGE 2 UPPER SKIN AT FR77, STGR 6L IAW EMB 145 SRM 53-32-01 REF STEP 9 AND PIEDMONT EO1-53-25-0286.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH CENTER SEAT TRACK #2 HAS GOUGES AND CORROSION IN NUMEROUS AREAS ALONG ENTIRE LENGTH. R&R LH ENTER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LAV R/H FLOOR SUPPORT IS CORRODED. R&R LAV R/H FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

REAR FUSELAGE 2 SKIN AT FR77 AND BETWEEN STGR 6R 7R AROUND A RIVET HEAD HAS A POSSIBILITY CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR77 AND BETWEEN STGR 6R-7R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0285.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

REAR FUSELAGE 2, SKIN AT FR77 AND BETWEEN STGR 5R/6R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2, SKIN AT FR77 AND BETWEEN STGR 3R/4R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0285.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

RH CENTER SEAT TRACK #1 HAS GOUGES AND CORROSION IN NUMEROUS AREAS ALONG ENTIRE LENGTH. R&R RH CENTER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

REAR FUSELAGE 2, SKIN AT FR78 AND BETWEEN STGR 6R-7R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR78 AND BTWEEN STGR 6R/7R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0385.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH #2 FLOOR SILL CORRODED IN NUMEROUS AREAS. R&R LH #3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 300) · airframe 52,025 hrs · 49,059 cycles

WHILE PERFORMING NDT INSPECTION AT AREA JUST FORWARD OF RUDDER 1, FOUND THAT THE VERTICAL STAB TRAILING EDGE RH SKIN PROFILE JUST ABOVE RUDDER 1 LOWER HINGE FITTING IS CRACKED. INSTALLED REPAIR PARTS ON VERTICAL STAB TRAILING EDGE RH SKIN PROFILE JUST ABOVE RUDDER 1 LOWER HINGE FITTING IAW EDT2025-145-926363 AND PIEDMONT EO1-55-25-0267.

Part: SUPPORT — CRACKED (ZONE 800) · airframe 52,025 hrs · 49,059 cycles

FOUND CRACK ON BAG DOOR LOWERING MECHANISM SUPPORT AT FR61. R&R BAG DOOR LOWERING MECHANISM SUPPORT AT FR61 IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

CARGO DOOR LOWERING MECHANISM AFT SUPPORT LOCATED BETWEEN FR67 AND FR68 HAS A CRACKED BRACKET. R&R CARGO DOOR LOWERING MECHANISM AFT SUPPORT BRACKET BETWEEN FR67 AND FR68 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH #3 FLOOR SILL CORRODED IN NUMEROUS AREAS. R&R LH #3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

CORRODED SHEAR CLIP IN CARGO BAY ON FR62 AND BETWEEN STGR 19R/20R. R&R SHEAR CLIP IN CARGO BAY ON FR62 AND BETWEEN STGR 19R/20R IAW EMB SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

REAR FUSELAGE 1 LH UPPER SKIN RIVET AT FR76, STRG 6L IS POSSIBLE CRACKED. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 1LH UPPER SKIN AT FR 76 STRG 6L IAW ETD2025-145-926199 / EO1-53-25-0283.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

REAR FUSELAGE 2, SKIN AT FR77 AND BETWEEN STGR 3R/4R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR77 AND BETWEEN STGR 3R/4R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0285.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

CENTER OMGA BEAM FLOOR SUPPORT IS CORRODED BETWEEN FR.56-57. R&R CENTER OMGA BEAM GUSSET BETWEEN FR.56-57 IAW EMB 145 SRM 51-40-02.

Part: BEAM — CORRODED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

CARGO DOOR CUTOUT LOWER BEAM TO FR65 PROFILE IS CORRODED. R&R CARGO DOOR CUTOUT LOWER BEAM TO FR65 PROFILE IAW EMB 145 SRM 51-40-02.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,025 hrs · 49,059 cycles

CARGO DOOR CUTOUT LOWER BEAM TO FR65 PRIFILE IS CORRODED. R&R CARGO DOOR CUTOUT LOWER BEAM TO FR65 PROFILE IAW EMB 145 SRM 51-40-02.

Part: BEAM — CORRODED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

CARGO DOOR CUTOUT LOWER BEAM HAS MULTIPLE CORROSION SPOTS. R&R CARGO DOOR CUT-OUT LOWER BEAM IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

RH #2 FLOOR SILL CORRODED IN NUMEROUS AREAS. R&R RH #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,025 hrs · 49,059 cycles

CARGO DOOR CUTOUT LOWER BEAM HAS MULTIPLE CORROSION SPOTS. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

L/H LOWER SEAT TRACK #5 HAS CORROSION IN MULTIPLE AREAS. R&R LH LOWER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

R/H LOWER SEAT TRACK #4 HAS CORROSION IN MULTIPLE AREAS. R&R RH LOWER NUMBER 4 SEAT TRACK IAW EMB 145 AMM 53-01-06 SRM 53-00-11AD.

Part: REPAIR — INCORRECT (ZONE 300 ELEV) · airframe 52,025 hrs · 49,059 cycles

LH ELEVATOR ACCESS PANEL 335HB CUTOUT INTERNAL REPAIR COUBLER HAS NO REPAIR INFORMATION. ACCOMPLISHED PERMANENT REINFORCING REPAIR ON LH ELEVATOR ACCESS PANEL 335HB CUTOUT IAW ETD2025-145-925992 REV-A AND PIEDMONTEO1-55-25-0271.

Part: REPAIR — INCORRECT (ZONE 300) · airframe 52,025 hrs · 49,059 cycles

RH ELEVATOR EXTERIOR UPPER SKIN #2 HINGE CUTOUT REPAIR DOUBLER HAS NO REPAIR INFORMATION. C/W PERMANENT REPAIR ON THE RH ELEVATOR UPPER SKIN #2 HINGE CUTOUT IAW ETD2025-145-925991 REV B AND EO1-55-25-0272.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH #7 FLOOR SILL IS CORRODED. R&R LH #7 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,025 hrs · 49,059 cycles

LH #6 FLOOR SILL IS CORRODED. R&R LH #6 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: INTAKE — CORRODED (ZONE 400) · airframe 52,025 hrs · 49,059 cycles

LEFT ENGINE AIR INTAKE LIP IS CORRODED. R&R LT ENGINE AIR INTLET ASSEMBLY IAW EMB 145 AMM 71-60-01.

Part: DRAG BRACE — CORRODED (NLG) · airframe 52,025 hrs · 49,059 cycles

CORROSION ON NLG DRAG BRACE LH LOWER HALF BEARING CAP. R&R NLG DRAG BRACE LH LOWER HALF BEARING CAP IAW PIEDMONT WORK CARD 53-20-06

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 52,025 hrs · 49,059 cycles

FUSELAGE SERVICE DOOR CUT-OUT AT FR-22 AND BETWEEN STGR 15R/16R HAS CORROSION. REPAIRED FUSELAGE SERVICE DOOR CUT-OUT AT FR-22 BETWEEN STGR 15R/16R IAW EMB 145 SRM 53-00-04 REF ITEM 16, FIG 208.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,368 hrs · 48,305 cycles

BLD 2 VLV FAIL EICAS MSG APPEARS WHEN T/O THRUST APPLIED. MSG EXTINGUISHED WHEN THRUST REDUCED. REJECTED TAKEOFF. HISTORY: YES FACT 22JUN23 23:27 PHL FOLLOWED THE FIM TASK 36-11-00-810-806-A. R&R HIGH STAGE PRESSURE SWITC #2 PER AMM 36-11-07, GROUND RAN. OPS CHECK GOOD, A/C OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,363 hrs · 48,299 cycles

BLEED 2 VBALVE FAIL ON TAKEOFF. REJECTED TAKEOFF. FACT 21JUN23 14:50 PHL R&R #2 ENGINE BLEED VALVE IAW EMB 145 MM 36-11-05 OPS CHECK LEAK CHECK GOOD AT THIS TIME. OK FOR SERVICE

Part: NOT ENTERED — NOT ENTERED · airframe 50,596 hrs · 47,474 cycles

PDIS 646 31-50 2908992 01FEB23 PHL CLOSE NO TAKEOFF CONFIG MESSAGE WHEN THRUST LEVERS ADVANCE. PARKING BRAKE OFF AND PARKING BRAKE LIGHT IS ILLUMINATED. ABORTED TAKEOFF LESS THAN 20 KNOTS FACT 01FEB23 12:14 PHL R/R PARKING BRAKE PRESS SWITCH IAW EMB MM 32-44-07 & R/R CANNON PLUG TO PARKING BRAKE PRESS SWITCH AS REQ'D. OPS CHECK LEAK CHECK GOOD AT THIS TIME.

Part: ENGINE — FAILED (NR 1) · airframe 50,289 hrs · 47,153 cycles

ON TAKEOFF ROLL AT APROX 10 KNOTS OIL PRESSURE ROSE AND A POP WAS HEARD. ENGINE ROLLED BACK WITH E1 OUT AND E1 NO DISPATCH MESSAGES DISPLAYED. ENGINE REMOVED AND REPLACED.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,765 hrs · 46,550 cycles

STRONG ODOR IN CABIN AFTER ENGINE 2 START. INSP PACKS 1 AND 2 AND PERF GVI OF E2. NO DEFECTS NOTED. PERF ENGINE RUNS WITH BOTH ENGINES, USING APU AND BOTH BLEEDS. NO DEFECTS OR SMELLS NOTED AT THIS TIME

Part: RELAY — FAILED · airframe 48,143 hrs · 44,716 cycles

ON CLIMB OUT PITOT 1 INOP CYCLED ON AND OFF FREQUENCY INCREASED ON DECENT. FACT 01SEP21 21:03 CLT T/S USING FIM TASK 30-31-00-410-801-A BLOCK 1-36 R&R RELAY K0111, REMOVED INSP + REINSTALLED RELAY K0056 R&R ANTI ICE PANEL. PERFORMED OPS CHECK 30-31-00 + FAIL STEP J1(C1) NO FIX. SLAVED IN #1 PITOT TUBE AND #4 STATIC PORT NO FIX. R&R RELAY K0111 AND PERFORM OPS CHECK IAW AMM 30-31-00-700-803-A. NO FIX. ON STEP (J)(1)(C) ONLY PITOT 2 AND 3 CAUTION MSG IS DISPLAYED WHEN THE N2 SIGNALS 2A C/B IS PULLED OK FOR SERVICE. PREVIOUS HISTORY: R/R RELAY K0053. R/R CURRENT SENSOR. R+R PITOT 1. R&R'D RELAY K0064. R&R RELAY K0056. USING FIM 30-31-00-810-801-A, BLOCKS 1,2,3,20,21,22,38,FOUND RELAY K0053 TO BE DISCOLORED.MEASURED CURRENT DRAW OF SYSTEM AT 7.5A.HAD GOOD GROUND AT PIN A-20 OF J1019 AT DAU#1 RACK CONNECTOR WITH PITOT 1 SYSTEM OPERATING. CHECK P0763 + P0087 FOR CORROSION,NONE FOUND.CHANGED RELAY BASE XK0053 + RELAY K0053. TRIMMED OFF B2 OF XK0056,(HAD NO PIN TENSION AT ALL) AND REPINNED. REPLACED K0056. SEE LOGPAGE 239931 SEQ#1 FOR REST OF SIGN OFF. OPS CHECK GOOD IN REF TO 34-13-00-05.TRIMMED OFF B2 OF XK0056,(HAD NO PIN TENSION AT ALL) AND REPINNED. REPLACED K0056. SEE LOGPAGE 239931 SEQ#1 FOR REST OF SIGN OFF. OPS CHECK GOOD IN REF TO 34-13-00-05.

Part: DOOR FRAME — CORRODED (RT ESCAPE HATCH) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

RH CABIN ESCAPE HATCH LWR FRAME CORRODED AROUND AFT GUIDE STRIP .... REMOVED AND INSTALLED NEW RH CABIN ESCAPE HATCH LWR FRAME AFT GUIDE STRIP IAW EMB145 SRM 51-40-02.

Part: BRACKET — DENTED (CARGO DOOR) · airframe 47,551 hrs · 44,055 cycles

CARGO DOOR LWR OUTER BRACKET DENT .... RAR CARGO DOOR LOWER OUTER PROFILE IAW EMB-145 SRM 51-40-02, 51-20-03.

Part: BRACKET — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

CARGO DOOR LWR INNER BRACKET CORRODED AROUND NUT PLATE HOLE .... RAR CARGO DOOR LWR INNER BRACKET IAW EMB 145 SRM 51-40-02, AND RAI THE CARGO DOOR HOLD OPEN ROD TO FOM IAW EMB 145 AMM 20-10-01.

Part: GUSSET — CORRODED (LAVATORY) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LAV RH BEAM GUSSET CORRODED .... REMOVED AND REPLACED LAV RHBEAM GUSSET IAW EMB145 SRM 51-40-02

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 47,551 hrs · 44,055 cycles

CARGO DOOR ROTATING HANDLE CUTOUT CRACKED AT AFT UPPER CORNER (MARKED)....INSTALLED DOUBLER AND FILLER FOR REPAIR OF CARGO DOOR EXTERNAL SKIN AT EXTERNAL ROTATING HANDLE CUTOUT IAW ETD2021-145-010311 AND EO1-52-21-0093.

Part: RIB — CRACKED (RT WING) · airframe 47,551 hrs · 44,055 cycles

RH WING RIB 21 CRACKED INSIDE PANEL 651CB....ACCOMPLISHED REPAIR OF RH WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 AND PIEDMONT EO1-57-21-0100.

Part: HOUSING — CRACKED (CRGO DOOR HANDLE) · airframe 47,551 hrs · 44,055 cycles

CARGO DOOR EXTERNAL HANDLE CUP CRACKED AT AFT UPPER CORNER .... RAR CARGO DOOR EXTERNAL HANDLE CUP IAW EMB-145 SRM 51-40-02 AND PIEDMONT EO1-52-21-0093

Part: DOOR FRAME — CORRODED (ESCAPE HATCH) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LH CABIN ESCAPE HATCH LWR FRAME CORRODED AROUND AFT GUIDE STRIP (MARKED)....REMOVED AND INSTALLED NEW LH CABIN ESCAPE HATCH LWR FRAME AFT GUIDE STRIP IAW EMB145 SRM 51-40-02.

Part: SKIN — CRACKED (FRM 78 S3-4R) · airframe 47,551 hrs · 44,055 cycles

INVESTIGATE POSSIBLE SKIN CRACK AT FR 78 BETWEEN STGRS 03R/04R (MARKED)...PERFORMED PT INSPECTION IAW EASI NDTM SKIN CRACK FOUND AT FASTENER RH FRAME 78 CRACK ENDS MARKED, CRACK APPROX. 1/2" LONG....INSTALLED SERVICEABLE REPAIR DOUBLER, UPPER AND LOWER FILLER AT FRAME 78, BETWEEN STRINGER 03R AND 04R IAW ETD2021-145-010521 AND PIEDMONT EO1-53-21-0096

Part: SUPPORT — CORRODED (WASTE VALVE) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

TOILET WASTE VALVE SUPPORT (LAV BUCKET) CORRODED .... REMOVED AND INSTALLED SERVICEABLE LAV BUCKET IAW EMB145 SRM 51-40-02.

Part: SKIN — DENTED (FRMS 58-59 S7L) · airframe 47,551 hrs · 44,055 cycles

DMT 23 DENT ON LH FUSELAGE BETWEEN FRAMES 58 AND 59 AND STRG. 7L AND 8L REPAIRED PER EO1-53-20-0126 WITHIN 1700 FLIGHT HOURS ACCOMPLISH A PERM. REPAIR....FABRICATED, PREPPED AND INSTALLED SERVICEABLE REPAIR DOUBLER AND FILLER ON LH FUSELAGE BETWEEN FR 58-59 AT STR 7L IAW EMB 145 SRM 53-24-01, ITEM 2, FIG 208 SHEET 3 AND EO1-53-21-0090.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

SERVICE DOOR FWD SILL AFT NUTPLATE CORRODED .... INSTALLED DOUBLER REPAIR ON THE SERVICE DOOR FWD SILL ON THE AFT END IAW EMB 145 SRM 53-21-10RE ITEM 5, FIG 204 SHEET 1.

Part: NUT PLATE — MISSING (RUDDER) · airframe 47,551 hrs · 44,055 cycles

DMT 01 PROTRACTOR NUT PLATE MISSING TRAILING EDGE RUDDER LH SIDE, REPLACE WITHIN 5000 FC PER SRM 55-40-01....FABRICATED, PREPPED, AND INSTALLED REPAIR DOUBLER IAW ETD2021-145-009971, EMB 145 CPM 51-21-05 AND PIEDMONT CPM BULLETIN 51-02 AND PIEDMONT EO1-55-21-0092.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 47,551 hrs · 44,055 cycles

CARGO DOOR INTERNAL LWR SKIN CHAFFED AT 5 LOCATIONS BETWEEN VB3 AND HB3 .... BLENDED AREAS AT VB2/HB3 AND VB3/HB4 FOUND TO BE OUT OF ALLOWABLE LIMITS IAW EMB 145 SRM 52-30-01. REMOVED DAMAGED PREVIOUS REPAIR DOUBLER AT HB4/FWD FRAME, PERFORMED 3 CUTOUTS ON CARGO DOOR INNER WEB AT HB4/FWD FRAME, VB2/HB3 AND VB3/HB4 AND FABRICATED AND INSTALLED 3 REPAIR DOUBLERS IAW EMB-145 SRM 52-30-01 RE ITEM 12. AND E01-52-21-0094

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LH OUTBD FLOOR SILL #3 IS PITTED .... BLENDED DAMAGE ON L/H #3 OUTBOARD FLOOR SILL AND FURTHER INVESTIGATION FOUND TO OUT OF LIMITS. IAW EMB145 SRM 53-22-10AD.REMOVED AND REPLACED LH OUTBD FLOOR SILL #3 IAW EMB145 SRM 51-40-02 AND SRM 51-20-01.

Part: FLOOR SUPPORT — CORRODED (LAVATORY) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LAV LH FLOOR SILL CORRODED AT LAV AFT BULKHEAD .... REMOVED AND REPLACED LAV LH FLOOR SILL AT LAV AFT BULKHEAD IAW EMB145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LH INBD #1 SEAT TRACK CORRODED AT FWD END .... REMOVED AND REPLACED LH INBD #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

RH OUTBD FLOOR SILL #1 IS PITTED .... RAR RH OUTBD FLOOR SILL #1 IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-03

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

RH OUTBD FLOOR SILL #3 IS PITTED .... BLENDED DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW EMB 145 SRM 53-23-10. REMOVED RH OUTBD FLOOR SILL #3 IAW EMB 145 SRM 51-40-02. DRILLED AND INSTALLED SERVICEABLE RH OUTBD #3 FLOOR SILL IAW EMB 145 SRM 51-20-03 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

RH CABIN #4 FLOOR SILL CORRODED. REMOVED AND REPLACED THE RH CABIN #4 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

RH OUTBD FLOOR SILL #2 IS PITTED .... REMOVED AND REPLACED NEW R/H OUTBOARD FLOOR SILL #2 TO IAW EMB 145 SRM 51-40-02

Part: FRAME — CORRODED (FRM 20) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

CROSSBEAM AT FR 20 CORRODED ....REMOVED AND REPLACED SERVICEABLE CROSSBEAM AT FR 20 IAW EMB145 SRM 51-40-02 AND SRM 51-20-01

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LH CABIN #4 FLOOR SILL CORRODED .... REMOVED AND REPLACED NEW L/H CABIN #4 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

CARGO DOOR LOWER FLOOR SILL CORRODED .... REMOVED AND REPLACED NEW CARGO DOOR LOWER SILL IAW EMB-145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 47,551 hrs · 44,055 cycles

LH #2 OUTBD FLOOR SILL IS PITTED .... LH #2 OUTBD FLOOR SILL IS PITTED. R & R LH #2 OUTBD FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: UPLOCK — FAULTY (LT MLG) · airframe 46,571 hrs · 42,964 cycles

RETURN TO FIELD LOUD BANGING IN N.L.G BAY. L/H MLG CYCLING. -CREW REPORTED L/H HYD PRESSURE CYCLING WITH GEAR. MAINTENANCE REMOVED AND REPLACED LH MAIN LANDING GEAR UPLOCK BOX IAW EMB AMM 32-33-10. OPERATIONAL/LEAK TEST SATISFACTORY. OK FOR SERVICE. AIRCRAFT RELEASED FOREVALUATION FLIGHT DUE TO: RTF FOR LOUD BANGING IN NOSE BAY. LH GEAR CYCLING REF LP 215204/2 MAINTENANCE ACTION COMPLETE SUBJECT TO SATISFATORY EVALUATION FLIGHT. CREW: EVAL FLIGHT IS SATISFACTORY.

Part: PROXIMITY SWITCH — FAULTY (MLG) · airframe 46,570 hrs · 42,960 cycles

PDIS 646 32-10 2152031 26MAR20 PHL CLOSE DURING GEAR RETRACT, LOUD THUMPING NOISE WITH L/H ML G INDICATION CYCLING BETWEEN UP AND IN TRANSIT. FACT 26MAR20 03:34 PHL R&R BOTH MLG UPLOCK BOX PROXIMITY SWITHCHES IAW AMM 32-61-01. EXTENDED AND RETRACTED LANDING GEAR IAW AM M 32-30-00. NO DISCREPAENCIES NOTED AT THIS TIME. OP S CHECK GOOD. SUPPLEMENTARY INFORMATION.... FLT NUMBER IS ACTUALLY 4914 ORIGINALLY REPORTED AS 9948

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 46,308 hrs · 42,680 cycles

LOST HYD SYS 2 FLUID IN FLIGHT. SUSPECT RAN AT EMPTY FOR OVER 15 MINUTES. INSPECTED AND FOUND #2 ENG HYD PUMP LEAKING. R&R #2ENG HYD PUMP REF AMM 29-10-03. DURING HYD PUMP R&R FOUND #2 ENG HYD PUMP ABG CARBON SEAL LEAKING. R&R #2 ENG HYD PUMP CARBON SEAL REF RR EMM 72-63-10-400-802 PER EDP INSP. 29-10-03. R&R #2 HYD MANIFIOLD CASE AND PRESSURE FILTERS REF. AMM 29-10-08. ALL LEAKS AND OPS CHECK GOOD ST THIS TIME.

Part: RELAY — MALFUNCTIONED (AOA) · airframe 46,013 hrs · 42,365 cycles

SPS 2 INOP DISPLAYED IN FLIGHT WITH AOA ANNUNCIATION ON F/O'S PFD. MAINTENANCE REMOVED AND REPLACED RELAYS K0357 AND K0359. PERFORMED STALL PROTECTION SYSTEM ADJUSTMENT AND TEST IAW E145 AMM 27-36-00 STALL PROTECTION SYSTEM OPERATION CHECK GOOD AT THIS TIME. ICEISPS INTERFACE CIRCUIT FUNCTIONAL CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 44,686 hrs · 40,847 cycles

PDIS 646 52-10 1846992 25APR19 PHL CLOSE AT APPOX 12K CREW NOTED LOUD WOOSHING/SQUEAL WITH SLOW PRESSURIZATION NOTED FACT 25APR19 18:13 PHL ADJUSTED MAIN DOOR OPEN/CLOSE HANDLE TO CORRECT POSITION PER AMM 52-18-00 AND CLEANED DOOR SEAL. MAIN DOOR REQRS OPS/LK CHECK.(SHORT SIGNED) PRESS. CHECK FAILED, SEE SEQ 3 FOR CONTINUATION.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 44,265 hrs · 40,373 cycles

PDIS 646 29-10 2033151 01FEB19 YYZ CLOSE LOSS OF #1 ENGINE HYDRAULIC PUMP PRESSURE ON LANDING ___ADDED INFO CAPT REPORTED LOSS OF NOSEWHEEL STEERING AND O/B BRAKES. HISTORY: . DFRL 02FEB19 23:53 YYZ R&RD #1 ENG HYD PUMP IAW AMM 29-10-03 YYZ MECH SHORT SIGN AP # 3717647. REQUIRES PRESSURE AND CASE DRAIN FILTER INSPECTION. HYD SERVICING LEAK CHECK AND OPS CHECK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,148 hrs · 40,234 cycles

PDIS 646 36-12 1660891 01JAN19 PHL CLOSE BLEED 1 VALVE CLOSED EICAS MESSAGE DISPLAYED AFTER TAKE OFF. CREW FOLLOWED QRH. MSG REMAINED. HISTORY: FACT 01JAN19 16:31 PHL GROUND RAN NR 1 ENGINE FOR 15 MINUTES. OPS CHECKED IAW AMM 36-11-05-700-802-A. OPS CHECK BLEED CHECK AND LEAK CHECK GOOD. NO OBVIOUS DEFECTS NOTED. NO MESSAGES DISPLAYED. OKAY FOR SERVICE.

Part: STRUCTURE — CRACKED (EMERGENCY LIGHT) · airframe 43,492 hrs · 39,468 cycles

RT #7 FLOOR EXTRUSION IS CRACKED. C/A-COMPLETE:REMOVED REPLACED RT #7 FLOOR EXTRUSION IAW AMM 33-50-12. SEE BOW 298426 FOR INSTALLATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,492 hrs · 39,468 cycles

LT #1 LIGHT STRIP EXTRUSION IS CRACKED. C/A-COMPLETE:REMOVED AND REPLACED LT #1 LIGHT STRIP EXTRUSION IAW AMM 33-50-12 ETN-EM-33-058. SEE BOW 298426 FOR INSTALLATION OPS CHECK.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

CROSSBEAM BETWEEN FR 37-38 IS CORRODED. C/A-COMPLETE:REMOVED CORRODED CROSSBEAM BETWEEN FR 37-38 POSITIONED DRILLED AND INSTALLED SERVICEABLE CROSS BEAM IAW ETN-EM-53-139 AND SRM 53-21-10.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

LT CENTER AISLE OMEGA BEAM CRACKED ON WEB AT FR33. C/A-COMPLETE:ACCOMPLISHED REPAIR OF LT CENTER AISLE OMEGA BEAM WEB AT FR33 IAW ERS-EM-53MR-3368.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

FLANGE ON LT CENTER AILSE OMEGA BEAM CORRODED BETWEEN FR. 33 AND 34. C/A-COMPLETE:ACCOMPLISHED REPAIR OF FLANGE ON LT CENTER AISLE OMEGA BEAM BETWEEN FR 33 AND 34 IAW ERS-EM-53MR-3368.

Part: LIGHT — CRACKED (CABIN) · airframe 43,492 hrs · 39,468 cycles

LT #6 LIGHT STRIP EXTRUSION IS CRACKED. C/A-COMPLETE:REMOVED REPLACED LT #6 LIGHT STRIP EXTRUSION IAW AMM 33-50-12 ETN-EM-33-058. SEE BOW 298426 FOR INSTALLATION OPS CHECK.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

CROSSBEAM AT FR 20 IS CORRODED. C/A-COMPLETE:REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AT FR20 IAW SRM 51-40-02, 53-21-10 ETN-EM-53-139.

Part: LIGHT — BROKEN (CABIN) · airframe 43,492 hrs · 39,468 cycles

#2 CENTER ISLE EMERGENCY LIGHT STRIP BROKEN AT LIGHT CONNECTION. C/A-COMPLETE:RAR #2 CENTER ISLE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW298426 TASK #1 FOR OPERATIONAL CHECK.

Part: LIGHT — CRACKED (CABIN) · airframe 43,492 hrs · 39,468 cycles

LT #2 LIGHT STRIP EXTRUSION IS CRACKED. C/A-COMPLETE:REMOVED REPLACED LT #2 LIGHT STRIP EXTRUSION IAW AMM 33-50-12 ETN-EM-33-058. SEE BOW 298426 FOR INSTALLATION OPS CHECK.

Part: LIGHT — CRACKED (CABIN) · airframe 43,492 hrs · 39,468 cycles

LT #5 LIGHT STRIP EXTRUSION IS CRACKED. C/A-COMPLETE:REMOVED REPLACED LT #5 LIGHT STRIP EXTRUSION IAW AMM 33-50-12 ETN-EM-33-058. SEE BOW 298426 FOR INSTALLATION OPS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

LT UPPER AFT FUSELAGE SKIN CRACKED IN 2 PLACES; PLACE1: JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L CRACK IS APPROX. 3/8' LONG (MARKED), PLACE 2:SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, CRACK IS APPROX. 1/4" LONG. EASI #8071 USED WITH 50-500KHZ PROBE, FREQ=400 KHZ, V-GAIN=78.0, H-GAIN=65.0, LPF=100, ANGLE=134.-C/A-COMPLETE:PERFORMED DOUBLER REPAIR AT LT UPPER FR. 75 ABOVE STRINGER 2 IAW SRM 53-31-01.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

CROSSBEAM AT FR 18 IS CORRODED. C/A-COMPLETE:RAR CROSS BEAM AT FRAME FRAME 18 IAW SRM 51-40-02 AND ETN-EM-53-139.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,492 hrs · 39,468 cycles

RT UPPER AFT FUSELAGE SKIN CRACKED IN 2 PLACES;PLACE1: JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R CRACK IS APPROX. 3/8' LONG (MARKED), PLACE 2:SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2R ON FRAME 75, CRACK IS APPROX. 1/4" LONG. EASI #8071 USED WITH 50-500KHZ PROBE, FREQ=400 KHZ, V-GAIN=78.0, H-GAIN=65.0, LPF=100, ANGLE=134. C/A-COMPLETE:ACCOMPLISHED DOUBLER FILLER REPAIR AT FR 75 STR 2R IAW SRM 53-31-01.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 43,399 hrs · 39,363 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND RT LOWER ROLLER HARD TO MOVE. LUBRICATED MAIN CABIN DOOR ROLLERS AND OPC GOOD IAW AMM REF 52-10-01.

Part: HANDLE — DIRTY (MAIN DOOR) · airframe 43,401 hrs · 39,367 cycles

MAIN DOOR NOT OPENING PROPERLY. INSPECTED AND FOUND HANDLE OF MAIN DOOR REQUIRING CLEANING AND LUBING. OPS CHECK GOOD IAW AMM 52-18-05.

Part: ACM — FAILED (AC BAY) · airframe 43,398 hrs · 39,362 cycles

EXPERIENCED A BURNING SMELL IN THE COCKPIT WITH A SMOKY HAZE BUILDING IN THE COCKPIT, DISSIPATED AS WE DESCENDED. PERFORMED TROUBLESHOOTING PER FIM 21-20-00. FOUND NR 1 PACK ACM TO HAVE FAILED. REMOVED AND REPLACED NR 1 PACK ACM PER AMM 21-51-03. OPC GOOD. NO SMOKE SMELL

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 42,800 hrs · 38,800 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (SERVICE DOOR) · airframe 41,871 hrs · 37,967 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-50-09-000-801-A, AND 33-50-09-400-801-A.. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 40,970 hrs · 37,141 cycles

TURBULACE DURING DECENT HAD LG AIR/GROUND FAIL. QRH PENALTY APPLIED, NORMAL LANDING, EICAS MESSAGE, LG AIR/GROUND FAIL REMOVED AT TOUCHDOWN. INSPECTED WOW SWITCHES, INSURED CONNECTORS SECURE IAW AMM 32-63-05, ALL CONNECTORS SECURE NO FURTHER DEFECTS NOTED.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 40,946 hrs · 37,120 cycles

LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AT 8000FT. WHILE FOLLOWING FIM TASK 32-63-00, FOUND THE LT MLG NR 2 PROXIMITY SWITCH AND RT NR 1 PROXIMITY SWITCH GAPS WERE OUT OF LIMITS ADJUSTED IAW AMM 32-63-05. REMOVED AND REPLACED THE RT MLG WOW NR 1 PROXIMITY SWITCH AND CORRECTED THE GAP IAW AMM 32-63-01 AND 32-63-05. OPS CHECKED NORMAL. COMPLIED WITH LANDING GEAR EXTENSION AND RETRACTION CHECK IAW AMM 32-30-00. SYSTEM OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (LT MLG) · airframe 40,873 hrs · 37,070 cycles

LG AIR /GND FAIL CAUTION MSG WHILE CLIMBING THROUGH FL 300 "TRANSFERRED TO NRWC 646-MIA-02812". FOLLOWING FIM TASK 32-63-00-810-806A, LANDING GEAR LEFT WOW PROX SW FAIL MESSAGE ON CMC, REMOVED AND REPLACED LEFT MLG DOWN LOCK PROXIMITY SW POSITION B, OPERATIONAL TEST SATISFACTORY ALL IAW AMM 32-61-02-400-801A.

Part: METERING UNIT — FAILED (NR 1 ENGINE) · airframe 40,379 hrs · 36,683 cycles

FUEL LEAKING OUT OF NR 1 ENGINE NACELLE. REMOVED AND REPLACED FPMU NR 1 IAW AMM 73-21-01. OPS CHECK GOOD NO LEAKS NOTED

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 38,984 hrs · 35,405 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE OUTSIDE. R & R UPPER AND LOWER FWD TEFLON GUIDES AND ADJUSTED THE FWD UPPER ROLLER IAW AMM 52-18-00. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 39,003 hrs · 35,419 cycles

EMERGENCY EXIT SIGN AFT OF RT OVERWING EXIT INOPERATIVE. FOUND ON CLOSE-UP. R & R EMERGENCY EXIT SIGN AFT OF RT OVERWING EXIT IAW AMM 33-50-13, CHECK GOOD.

Part: RIB — CRACKED (RT WING) · airframe 39,003 hrs · 35,419 cycles

RIGHT RIB 5 CRACKED AT THE AFT LARGE LIGHTNING HOLE. ACCOMPLISHED PERMANENT REPAIR TO RT RIB 5 IAW ERS-EM-57MR-648 01 AND ERS-EM-57MR-648.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,003 hrs · 35,419 cycles

SERVICE DOOR AFT SILL HAS CORROSION AROUND FWD NUTPLATE. REMOVED CORROSION FROM SERVICE DOOR, AROUND SILL AND NUTPLATE, REPLACED IAW SRM 51-40-09.

Part: FRAME — GOUGED (FUSELAGE) · airframe 39,003 hrs · 35,419 cycles

SIDEWALL PANEL SUPPORT BETWEEN STR-13R, FRAME 65 GOUGED. REPAIRED FRAME 65 LAW SRM 51-40-02, 51-20-01 AND 53-00-04.

Part: WIRE — BROKEN (CABIN) · airframe 39,003 hrs · 35,419 cycles

LEFT NR 4 EMERGENCY LIGHT STRIP HAS BROKEN WIRE. FOUND ON OPEN-UP, R & R LEFT NR 4 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: YOKE — CRACKED (LT PYLON) · airframe 39,003 hrs · 35,419 cycles

LEFT ENGINE FWD LOWER YOKE FWD FITTING CRACKED. REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,983 hrs · 35,404 cycles

EMERGENCY EXIT SIGN AFT OF RT OVERWING EXIT INOPERATIVE. R & R EMERGENCY EXIT SIGN AFT OF RT OVERWING EXIT IAW AMM 33-50-13, OPS CK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 38,983 hrs · 35,404 cycles

LEFT NR 4 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. R & R LT NR 4 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CK GOOD IAW AMM 33-50-00.

Part: ELECTRONIC UNIT — FAULTY (LANDING GEAR) · airframe 38,816 hrs · 35,252 cycles

NO LG IN TRANSIT DURING RETRACTION OR EXTENSION. WITH 3 GREEN UP & UP SELECTED RMU SHOWED LG DOWN & LOCKED. AFTER FURTHER INVESTIGATION FOUND LGEU TO BE AT FAULT. R & R LGEU IAW AMM 32-32-01. OPERATIONS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 38,753 hrs · 35,195 cycles

CAPTAIN FLASHLIGHT INOPERATIVE. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,303 hrs · 34,806 cycles

AFT EMER FLOOR LIGHTING STRIP INOPERATIVE. R & R AFT EMER FLOOR LIGHTING STRIP. OPERATIONS CHECKED GOOD IAW AMM 33-50-12.

Part: WIRE HARNESS — DAMAGED (NLG DOWNLOCK) · airframe 37,966 hrs · 34,466 cycles

AFTER TAKEOFF & ROTATION & GEAR RETRACTION A LOUD & RAPID CLANKING NOISE EMANATING FROM FLIGHT DECK. R & R NR 2 NLG DOWNLOCK PROX HARNESS & PROX SWITCH IAW AMM 32-61-02. OPERATIONS CHECKED GOOD IAW NRWC 646-DFW-02207 FOR DETAILS.

Part: BUSHING — WORN (RAM AIR VALVE) · airframe 37,910 hrs · 34,413 cycles

AFTER TAKEOFF A VERY LOUD CONTINUOUS & RANDOM CLACKING OR SPARKING SOUNDS WERE IMMEDIATELY HEARD IN THE COCKPIT. FLIGHT RETURNED WITHOUT INCIDENT. TRANSFERRED TO NRWC 646-ABI-02199. R & R BUSHINGS TO RAM AIR VLV & ADJUSTED LINEAR ACTUATOR IAW AMM 21-25-03. NO FURTHER DEFECTS NOTED. OPERATIONS CHECKED GOOD. SEE NRWC 646 ABI-02199 FOR CERTS & TURNOVER.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,758 hrs · 34,271 cycles

FORWARD EMER LIGHT EXIT SIGN INOPERATIVE. R & R NR 1 INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,710 hrs · 34,228 cycles

AFT CEILING EMER LIGHT AT PANEL 263 ALC INOPERATIVE. R & R EMER LIGHT BATTERY & CHARGER AT ROW 15 CEILING IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW AMM 33-50-00. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 13314.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,816 hrs · 33,387 cycles

DURING PS2 CHECK, FOUND EMER LIGHTS NOT ILLUMINATING, FLOOR STRIPS 6, 7 & 8. R & R NR 4 BATTERY POWER SUPPLY IAW MM 33-50-04. R & R NR 4 BATTERY IAW MM 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY, PN BA5-0933-901 & SN C01447.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 36,219 hrs · 32,849 cycles

CAPTAINS COCKPIT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 33-50-16. FLASHLIGHT CHECKED GOOD.

Part: PUMP — FAILED (LT ENGINE) · airframe 36,200 hrs · 32,837 cycles

ENGINE 1 HYD FAIL. COMPLIED WITH AOM VOL 1, LOWERED GEAR ON FINAL. NORMALLY HYD 1 ENG FAIL MSG WENT AWAY. REMOVED & INSTALLED NEW HYD PUMP 1 ENG IAW AMM 29-10-03. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,190 hrs · 32,830 cycles

AFT CABIN EMER FLASHLIGHT HOLDER BROKEN. R & R AFT EMER FLASHLIGHT HOLDER IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,179 hrs · 32,819 cycles

SEAT 3 & 4 FLOOR EMER LIGHT STRIP INOPERATIVE. DEFERRED IAW MEL 33-30. R & R FWD AMBER FLOOR PROXIMITY LIGHT STRIP EMER AMM CH 33-50-12. MEL RESTORED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 35,890 hrs · 32,598 cycles

FLIGHT ATTENDANT`S EMER FLASH LIGHT CRADLE BROKEN. R & R FLIGHT ATTENDANT`S EMER FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 35,567 hrs · 32,316 cycles

FORWARD BELLY FAIRING CRACKED. REPAIRED FWD BELLY FAIRING IAW ERS-ERS-EM-5300-741.

Part: UNKNOWN — ODOR · airframe 35,240 hrs · 31,995 cycles

SMELL OF ELEC BURNING DURING DESCEND & PARKING. COMPLIED WITH ETN-EM-72-034, PERFORMED ENG RUNS & INSPECTIONS OF ELEC AREAS, FOUND NO DAMAGE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

FOUND THE NR 1 LT AISLE PROXIMITY LIGHT STRIP CONNECTOR ON ACFT SIDE BROKEN OFF. REPAIRED NR 1 AISLE LIGHT STRIP CONNECTOR SP9019 ACFT SIDE IAW SWPM 20-00-03, 20-21-00 & WM 91-10-02.

Part: WIRE — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

NR 7 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. R & R NR 7 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

NUMBER 6 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. R & R NR 6 EMER LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

NUMBER 4 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. R & R NR 4 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

NUMBER 3 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. R & R NR 3 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

NR 5 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. R & R NR 5 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: FRAME — CHAFED (FUSELAGE) · airframe 34,386 hrs · 31,355 cycles

FRAME 15 & ADJACENT SHEAR CLIP CHAFED STRINGER 2R. PERFORMED PERMANENT REPAIR OF FRAME 15 & REPLACED SHEAR CLIP IAW ERS-EM-53MR-470.

Part: DOOR — CORRODED (CARGO BAY) · airframe 34,386 hrs · 31,355 cycles

CARGO DOOR CORRODED AT UPPER END FWD SCREW HOLE. PERFORMED PERMANENT REPAIR IAW ERS-EM-52MR-145.

Part: PIN — DISCONNECTED (FLASHLIGHT) · airframe 34,386 hrs · 31,355 cycles

PILOTS FLASHLIGHT HAS NO CHARGE. RECONNECTED PIN IAW WM 91-10-02 & SWPM 20-00-03, LED CHARGE LIGHT NOW ILLUMINATED, OPERATIONS CHECKED GOOD.

Part: PANEL — BROKEN (CABIN) · airframe 34,386 hrs · 31,355 cycles

NR 5 PROXIMITY LIGHT PANEL COVER LIP BROKEN. R & R NR 5 PROXIMITY LIGHT STRIP SIDEWALL ASSEMBLY IAW AMM 33-50-12. OPERATIONAL CHECKED GOOD.

Part: SHROUD — CORRODED (RT AILERON) · airframe 34,386 hrs · 31,355 cycles

RIGHT WING AILERON LWR SHROUD MOUNTING FLANGE OTBD 9 NUTPLATE HOLES HAVE CORROSION AROUND THE NUTPLATE HOLE. RT WING AILERON LWR SHROUD MOUNTING FLANGE OTBD 10 NUTPLATE HOLES HAVE CORROSION AROUND THE NUTPLATE HOLE FOUND TO BE ACCEPTED IAW ERS-EM-5700-151. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,386 hrs · 31,355 cycles

FUSELAGE EXTERNAL SKIN CRACKED AROUND 1 FASTENER FRAME 78 RT SIDE BELOW VERTICAL STAB. INSTALLED REPAIR BUSHING ON FUSELAGE EXTERNAL SKIN AT FRAME 78 ON RT SIDE BELOW VERTICAL IAW ERS-EM-5300-453.

Part: FASTENER — CORRODED (PITOT TUBE) · airframe 34,386 hrs · 31,355 cycles

LEFT PITOT TUBE HAS CORRODED HARDWARE. R & R LT PITOT TUBE HARDWARE IAW AMM 34-13-01STEPS 2J 2B & STEPS 3I 6.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 34,011 hrs · 31,020 cycles

FLIGHT ATTENDANT SAID MAIN CABIN DOOR STICKS & HARD TO OPEN. LUBRICATED ROLLERS IAW SMP, DOOR OPERATED NORMALLY.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 33,969 hrs · 30,988 cycles

FIRST OFFICER`S LANDED, INITIAL BRAKING 50% EFFECTIVENESS AT BEST, TRANSFERRED TO CAPTAIN AT 90 KTS, SAME ON CAPTAIN'S BRAKES 50% AT BEST. USED REVERSE THRUST TO SLOW DOWN, EICAS CAUTIONS CAME ON BRAKE DEGRADED & THEN BRAKE OTBD INOPERATIVE AT APPROXIMATELY 30 KTS. CAPTAIN FELT FULL BRAKING RE-ENGAGE. BLED ALL FOUR BRAKES IAW AMM-32-40-00 & PERFORMED THE RUN OF BRAKE FIELD ANALYZER SOFTWARE ALL FOUR BRAKES ARE WORKING NORMAL IAW 32-41-00.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,841 hrs · 30,104 cycles

FIRST CABIN FLOOR EMERGENCY PROXIMITY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT INVERTER NR 2 AND CHECKED GOOD.

Part: CONTROL PANEL — SMOKE (STALL PROTECTION) · airframe 32,759 hrs · 30,027 cycles

SMOKE SEEN COMING FROM STALL PROTECTION TEST PANEL. SMOKE AND ELECTRIC ODOR PRESENT IN COCKPIT. SMOKE ALSO SEEN COMING FROM STALL PROTECTION TEST BUTTON. R & R STALL PROTECTION PANEL IAW AMM 20-13-10. OPS CHECKED GOOD IAW AMM 27-36-00.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 32,166 hrs · 29,549 cycles

DURING B INSPECTION, FOUND EMERGENCY LIGHTS 4 AND 5 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT DC/AC INVERTER NR 5 IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,108 hrs · 29,499 cycles

DURING B-INSP, FOUND THE CENTER SECTION FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY BATTERY AND CHARGER ASSY IAW AE W/C 33-700-19. THE OPS CHECK WAS GOOD IAW AE 33-700-17. THE ACFT WAS RETURNED TO SERVICE.

Part: TAPE — DEPARTED · airframe 32,052 hrs · 29,460 cycles

SPEEDTAPE ON C/A SIDE HUMP SEAL CAME OFF ON THE CLIMBOUT FOLLOWED BY STRONG BURNED PLASTIC SMELL IN ACFT, REF TO NRWC 646-DFW-01255 AND 646-DFW-01259. REAPLLIED SPEED TAPE ON CAPT HUMP SEAL AND PERFORMED NR 1 ENGINE INLET INSPECTION. NO DAMAGE FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,629 hrs · 29,126 cycles

DURING MAINTENANCE INSPECTION FOUND ROW 12 RT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W REMOVED AND REPLACED ROW 12 RT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07, OPC CHECK GOOD IAW WC 33-700-17. THE AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — UNKNOWN (CABIN) · airframe 31,541 hrs · 29,055 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR DIFFICULT TO PUSH OUT OF FUSELAGE FRAME---DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH INSIDE HANDLE MAIN CABIN DOOR PULL TEST 52 18 00 820. FORCE WAS FOUND TO BE 40LBS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 31,465 hrs · 29,005 cycles

ON FLIGHT 2885 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR EXTERNAL HANDLE AND FUSELAGE ROLLERS. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 52 18 00(820-001). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 31,317 hrs · 28,887 cycles

ON FLIGHT 2867 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR ROLLERS IAW EMV MM 53-21-02, DOOR OPS CHECK SATISFACTORY IAW EMB MM 52-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 31,286 hrs · 28,861 cycles

ON FLIGHT 3335 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND LUBED IAW EMB AMM 52-11-00 AND THE OPERATIONAL CHECKS WERE GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUIDE — DIRTY (CABIN DOOR) · airframe 31,280 hrs · 28,855 cycles

ON FLIGHT 3226 THE FLIGHT ATTENDANT REPORTED THE 28,855 WAS HARD TO GET OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED THE MAIN CABIN DOOR GUIDES PER 52-11-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (ENTRY DOOR) · airframe 31,040 hrs · 28,675 cycles

ON FLIGHT 4323 THE FLIGHT ATTENDANT REPORTED THE MAIN ENTRY DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR EXTERNAL HANDLE. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 52 18 00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 30,967 hrs · 28,613 cycles

ON FLIGHT 3216 THE CREW REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED MAIN DOOR, CLEAN & LUBE IAW 52-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 30,518 hrs · 28,268 cycles

ON FLIGHT 3329 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT FOR THE FLIGHT ATTENDANT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (MAIN DOOR) · airframe 30,357 hrs · 28,136 cycles

ON FLIGHT 2740 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR HANDLE WAS HARD TO MOVE AND THE DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ONE ROLLER STICKY, CLEANED AND LUBED ROLLER. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 30,246 hrs · 28,050 cycles

ON FLIGHT 2795 THE CREW REPORTED THE MAIN CABIN PASSENGER DOOR WAS VERY DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEAN AND LUBE FRAME ROLLS OPEN AND CLOSE. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CAM — LACK OF LUBE (CABIN DOOR) · airframe 30,137 hrs · 27,964 cycles

ON FLIGHT 2845 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED BOTH CAMS PERFORMED FUNCTIONAL CHECK OF ACTUATING HANDLE IAW EMB 145 52-18-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BAR — OUT OF ADJUST (CABIN DOOR) · airframe 30,089 hrs · 27,932 cycles

ON FLIGHT 3392 THE FLIGHT ATTENDANTS REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN, IT APPEARED TO CATCH ON THE UPPER LEFT CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED 1 ADDITIONAL WASHER BETWEEN DOOR ARM FITTING NR 1 AND NR 2 PER ETN #EM-52-013R1 AND EMB 145-AMM 52-18-00. ADJUSTED FORWARD UPPER/LOWER BAR REF TO EMB AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (MAIN DOOR) · airframe 30,076 hrs · 27,920 cycles

ON FLIGHT 3387 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR ROLLERS PIN IAW AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,059 hrs · 27,908 cycles

DURING MAINTENANCE INSPECTION FOUND THE FUSELAGE TO HAVE CORROSION AT FRAME 13-14. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT AND INSTALLED DOUBLER IAW EO EM-53MR-2026. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — DAMAGED (CABIN) · airframe 30,067 hrs · 27,915 cycles

DURING B INSPECTION FOUND TWO CABIN EMERGENCY LIGHT STRIP EXTRUSIONS DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED TWO CABIN EMERGENCY LIGHT STRIP EXTRUSIONS TO THE RIGHT NR 2 AND NR 4 POSTION IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE. SUPPLEMENTAL INFORMATION--THE CORRECT DATE SHOULD BE 9-13-12

Part: WIRE — BROKEN (CABIN) · airframe 30,067 hrs · 27,915 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR EMERGENCY EXIT LIGHT ON THE FORWARD LOWER CORNER TO HAVE A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CONNECTOR ON SERVICE DOOR EMERGENCY EXIT LIGHT FORWARD LOWER CORNER IAW EMB 145 SWPM 20-21-00 STEP 6 AND SWPM 20-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — DAMAGED (CABIN) · airframe 30,059 hrs · 27,908 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 BATTERY CHARGER DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 30,067 hrs · 27,915 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT 251BF AND 251FF TO HAVE BROKEN CONNECTORS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LIGHT STRIP BROKEN CONNECTORS AT 251BF AND 251FF IAW EMB 145 WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,067 hrs · 27,915 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT 231GF HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CONNECTOR ON EMERGENCY LIGHT STRIP AT 231GF IAW EMB 145 SWPM 20-21-00 STEP 6 AND SWPM 20-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 30,060 hrs · 27,908 cycles

SKIN SPLICE BETWEEN FRAME 13 AND 14 STR 20-21R CORRODED. PERFORMED REPAIR TO SKIN SPLICE IAW EO-EM-53MR-2026.

Part: HOLDER — DAMAGED (EMERGENCY LIGHT) · airframe 30,059 hrs · 27,908 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY HOLDER ASSEMBLY DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY HOLDER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,991 hrs · 27,852 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLOOR LIGHT STRIP AT SEAT 1A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED 1A FLOOR PROXIMITY STRIP IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD PER WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WASHER — WORN (PAX DOOR) · airframe 29,602 hrs · 27,545 cycles

FLIGHT 4177, CREW REPORTED MAIN CABIN DOOR BINDS WHEN TRYING TO OPEN IT AFTER PRESSURIZATION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED WORN ACTUATING CAM WASHER PER MM 52-18-01. OPS CHECKED GOOD. REF NRWC NR 646-ORD-00846. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — LOW (NLG) · airframe 29,580 hrs · 27,532 cycles

ON FLIGHT 4276 THE CREW REPORTED THAT DURING ROTATION RECEIVED A "LDG AIR/GND FAIL" EICAS MESSAGE. THE MESSAGE IMMEDIATELY WENT AWAY. THE CREW DECLARED AN EMERGENCY. THE CREW RECEIVED THE SAME MESSAGE ON TOUCHDOWN/ROLLOUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED NOSE LANDING GEAR IAW EMB AMM 32-20-01. PERFORMED AN OPERATIONAL CHECK OF AIR/GROUND WEIGHT ON WHEELS SYSTEM IAW EMB AMM 32-63-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LATCH — LACK OF LUBE (LAVATORY) · airframe 28,764 hrs · 26,953 cycles

ON FLIGHT 2751 THE CREW REPORTED THE LAV EMERGENCY FIRE BOTTLE DOOR WON’T OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED/LUBED (REMOVED FOD) ON LATCHES FOR LAV EMERGENCY FIRE BOTTLE DOOR. OPENED & CLOSED MULTIPLE TIMES AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — LOOSE (CABIN DOOR) · airframe 28,482 hrs · 26,741 cycles

ON FLIGHT 3237 MAIN CABIN DOOR WAS DIFFICULT TO PUSH OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED PANEL ON MAIN DOOR THAT WAS COMING IN WAY WHILE OPENING THE DOOR.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,195 hrs · 26,530 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY STRIP LIGHTS FROM SEAT 12 TO AFT CABIN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER FOR STRIP FLOOR PROXIMITY LIGHTS IAW EMB-145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,185 hrs · 26,524 cycles

ON FLIGHT 9303 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. THE AIRCAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR FRAME ROLLERS IAW EMB 145 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD IAW EMB 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,167 hrs · 26,512 cycles

ON FLIGHT 3368 THE CREW REPORTED THE MAIN CABIN DOOR WAS EXTREMELY DIFFICULT TO OPEN BY THE FLIGHT ATTENDANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR ROLLERS IAW EMB MM 53-21-02. THE OPERATIONAL CHECK OF THE MAIN CABIN DOOR WAS WITHIN LIMITS IAW EMB MM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (HORIZ STAB) · airframe 2,813,226 hrs · 26,489 cycles

ON FLIGHT 2733 THE CREW REPORTED THAT ON DESCENT THEY LOST PITCH TRIM "PTRIM MAIN INOP". THE BACK UP TRIM WORKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ELECTRIC OPERATIONAL TEST OF HORIZONTAL STABILIZER IAW EMB 145 AMM 27-40-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 27,800 hrs · 26,258 cycles

ON FLIGHT 2971 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE DOOR HANDLE HAD TO BE HELD TO THE RIGHT BEFORE THE DOOR COULD BE OPENED. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN DOOR LOCK MECHANISM. THE OPERATIONAL CHECK WAS GOOD AS REQ PER 52-10-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 26,959 hrs

FLIGHT ATTENDANT IS HAVING DIFFICULTY OPENING MAIN CABIN DOOR. LUBED MAIN DOOR IAW EMB STANDARD PRACTICES AND OPS CHECK GOOD IAW EMB 145 AMM 52-18-00. HAD FA OPEN AND CLOSE, OPS CHECK AS ASSIGNED. NO DEFECTS NOTED.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 26,172 hrs · 25,048 cycles

ON FLIGHT 4152 THE CREW REPORTED THAT DURING THE CLIMB RECEIVED A LANDING GEAR, AIR GROUND FAIL MESSAGE ON EICAS. THE GEAR WOULD NOT RETRACT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS SWITCH IAW EMB MM 32-63-02. THE OPERATIONAL CHECK WAS GOOD. PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST AND THE CHECK WAS GOOD IAW EMB MM 32-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 26,171 hrs · 25,044 cycles

ON FLIGHT 4202 THE CREW REPORTED THE RECEIVED A LAND AIR GROUND FAIL MESSAGE AFTER TAKEOFF. THE LANDING GEAR DID NOT RETRACT. THE CAPTAIN ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB 145 AMM 32-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (PAX DOOR) · airframe 25,143 hrs · 24,246 cycles

DURING MAINTENANCE BASE VISIT FOUND PASSENGER DOOR SKIN GOUGED ON THE AFT EDGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH PERMANENT REPAIR OF DOOR SKIN IAW ENGINEERING ORDER EM-5200-261. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 25,143 hrs · 24,246 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 9 ON THE LEFT TO BE GOUGED BETWEEN STRINGER 9 ON THE LEFT AND 13 ON THE LEFT. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REPAIRED FRAME 9 LEFT UNDER LEFT DIRECT VISION WINDOW IAW EMB SRM 53-00-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,143 hrs · 24,246 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 29. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO LEFT OMEGA BEAM AT FRAME 29 IAW EMBRAER SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 25,039 hrs · 24,166 cycles

FOR FLIGHT 3348 DURING INSPECTION FOUND EMERGENCY LIGHT STRIP AT ROW 18 TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROW 18. THE OPERATIOAL CHECK WAS GOOD IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 294,451 hrs · 24,673 cycles

DURING MAINTENANCE BASE VISIT FOUND THE MAIN DOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED GROUND ON MAIN DOOR EMERGENCY LIGHT IN REFERENCE TO EMB 145 AMM TASK 33-50-06-400-802-A. THE OPERATIONAL CHECK WAS NORMAL. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 294,451 hrs · 24,673 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN IN FRONT OF SEATS 3B AND 3C TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXIT SIGN AT SEATS 3BC AND 3BC IAW EMB 145 AMM 33-50-13-000-801-A. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPLICE — DISCONNECTED (CABIN) · airframe 24,826 hrs · 23,988 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT ON THE SERVICE DOOR FRAME TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. WHIILE TROUBLESHOOTING A WIRE SPLICE WAS FOUND TO BE DISCONNECTED. RECONNECTED THE SPLICE AND PERFOMRED AN OPERATIONAL CHECK OF THE LAMP IAW EMB AMMTASK 33-50-09-400-802-A. NO PARTS REMOVED OR REPLACED. THE AIRCAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 24,610 hrs · 23,821 cycles

FOR FLIGHT 3366 DURING THE PREFLIGHT CHECK FOUND THAT THE NR 2 BAGGAGE SMOKE DETECTOR WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 CARGO COMPARTMENT SMOKE DETECTOR IAW AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · airframe 20,077 hrs · 19,952 cycles

DURING INSPECTION, FOUND CARGO DOOR SILL CORRODED. REPLACED SILL IAW EMBRAER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,077 hrs · 19,952 cycles

DURING CPCP INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,669 hrs · 18,573 cycles

ON FLIGHT 301H, CREW REPORTED WHILE CLIMBING THRU FL 280, BOTH CREW MEMBERS DETECTED AN ELECTRICAL BURNING ODOR. AIR COMING FROM GASPER VENTS WAS CLEAN WITH NO ODOR. AIRCRAFT DIVERTED TO EVV. AIRCRAFT REMOVED FROM SERVICE. PERFORMED NUMEROUS CHECKS IN THE FLIGHT DECK AND OVERHEAD PANELS AND IN THE CABIN. RAN AIRCRAFT. NO FURTHER BURN ODOR NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 15,438 hrs · 15,698 cycles

FRAME 81 CHAFED. REMOVED AND REPLACED FRAME IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 15,438 hrs · 15,698 cycles

STRINGER 19 FOUND CHAFED BETWEEN FRAMES 53 AND 54. BLENDED DAMAGE, PERFORMED NDT FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-24-02. AIRCRAFT RETURN TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ORD - FLT 4014 - LANDING GEAR LEVER DISAGREE WARNING ON EICAS ON TAKEOFF. APPLIED EMERGENCY PROCEDURES GEAR REMAIN DOWN WITH GREEN INDICATION. PLACED GEAR EMERGENCY SWITCH IN THE NORMAL POSITION AND PEFORMED GEAR EXTENSION AND RETRACTION TEST, IAW EMB 145, AMM 32-30-00. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. (M)

Part: SWITCH — BROKEN (A/C TEMP)

LRD - FLT 3595 - SMOKE IN CABIN DIVERTED TO LRD. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT AIR CONDITIONING SYSTEM. REPLACED OVER TEMPERATURE SWITCH ON NR 2 PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

DFW - PASSENGER REPORTED SMOKE IN CABIN WHILE SITTING AT THE GATE WITH APU RUNNING AND ENGINES SHUT DOWN. MAINTENANCE GROUND RAN ENGINES AND REPORTED NO SMOKE OR FUMES. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — GOUGED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LOWER FRAME 81 WAS FOUND GOUGED. REMOVED THE GOUGED FRAME. INSTALLED NEW FRAME IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTERS 51-20-01, 51-20-03, 51-40-02 AND 51-40-04. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON FRAME 20 AT THE LEFT OMEGA BEAM WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR PARTS TO REMOVE THE CORROSION. FABRICATED A DOUBLER, PLATE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 29, CHAPTERS 53-21-10 AND 51-40-02. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN MBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 51-20-01, 03, 51-40-02, 04, 06 AND EMB CPM, CPM 145/1132 REV 12 CHAPTER 51-21-04. (M)

Part: A/C PACK — MALFUNCTIONED (A/C BAY)

LBB - FLT 3390 - CREW REPORTED THE NR 2 PACK FAILED, WITH SMOKE PRESENT IN THE CABIN. THE LAVATORY SMOKE DETECTOR ACTIVATED, THE NR 2 PACK WAS DESELECTED AND THE CABIN SMOKE WENT AWAY WITH ONLY NR 1 RUNNING. PERFORMED OPERATIONAL CHECK OF NR 2 PACK WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

SMOKE IN CABIN REPORTED BY CREW AFTER APU START. APU PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. SEVERAL STARTS WERE PERFORMED WITH NO SMOKE NOTED. MEL WAS RESTORED AND AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

CLT - FLT 3807 - CREW REPORTED TWO OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY UNIT P/N 110049, AND BATTERY IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: APU — CONTAMINATED

PIT- FLT 4153 - CRWE REPORTED WITH APU RUNNING AND MAINTEANCE ON BOARD THE CABIN AND COCKPIT FILLED WITH SMOKE. CREW SAID IT SEEMED TO BE COMING FROM THE NR 2 PACK. MAINTENANCE RAN THE NR 2 PACK WITH THE APU AND FOUND NO ODOR. SUSPECT ANTI-ICE FLUID ENTERED THE APU BLEED SYSTEM. COULD NOT DUPLICATE DISCREPANCY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOND TO BE CORRODED BELOW SRM LIMITS AROUND A FASTENER HOLE. BLENDED THE CORRODED AREA AND PERFORMED NON DESTRUCTIVE TESTING WITH NO CRACK INDICATIONS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 21) CHAPTER 51-40-02/06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE NR EM-53-036R1. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACKS NOTED. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145-1142, REV 21, CHAPTER 53-24-02 FIGURE 201. (M)

Part: GUSSET — CORRODED (FUSELAGE)

ABI - FOUND FORWARD DIAMOND GUSSET CORRODED. REMOVED AND REPLACED GALLEY AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

ABI - FOUND CENTER BEAM RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE CENTER BEAM RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. FORWARD DIGITAL CENTER 2 INCH AFT OF COCKPIT WALL CORRODED. BLENDED, INSPECTED AND ACCEPTED AS IS IAW EMB GS 3196/01. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND SERVICE DOOR AFT SILL CORRODED FROM FRAME 21 TO 23. REMOVED AND REPLACED AFT DOOR SILL IAW EMB 145 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND FORWARD CENTER DIGITAL 2 INCH AFT OF COCKPIT WALL CORRODED. REPAIRED CENTER DIGITAL IAW EMB REPAIR STATEMENT GST 3196/01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND AFT PAX DOOR FLOOR SUPPORT CORRODED. REPAIRED AFT PAX DOOR FLOOR SUPPORT IAW EMB REPAIR STATEMENT GST-3196/01. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND CENTER BEAM AT FRAME 21 CORRODED. REPAIRED CENTER BEAM AT FRAME 21 IAW EMB REPAIR STATEMENT GST-3196/01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND CENTER BEAM GUSSET CORRODED AND CHAFED. REMOVED AND REPLACED GALLEY CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-22. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

MEM - FLT 4265 - BOTH CAPTAIN AND F/O PITCH TRIM MASTER WARNING LIGHT ILLUMINATED DURNG CLIMB AND CRUISE. RESET AIRCRAFT ELECTRICAL SYSTEM TRIM SYSTEM IAW AMM. OPS CHECK GOOD. (M)

Part: SMOKE — DETECTED (CABIN) · airframe 969 hrs · 1,054 cycles

EVV - FLT 4101 - FLIGHT ATTENDANT REPORTED SMOKE SMELL IN CABIN. INSPECTED CABIN WITH APU AND PACKS ON, FULL HOT, FULL COLD, FOUND NO DEFECTS. NO SMOKE OR FIRE DAMAGE NOTED. OPERATIONAL CHECK SYSTEM IAW AMM, FOUND NO DISCREPANCIES. AIRCRAFT RETURNED TO SERVICE. (X)