N739AE

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,108 hrs · 22,630 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT BULB IAW EMB 135 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (FLASHLIGHT) · airframe 26,108 hrs · 22,630 cycles

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT LEFT EMERGENCY FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT COCKPIT EMERGENCY FLASHLIGHT IAW EMB 135 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,933 hrs · 22,487 cycles

ON FLIGHT 4507 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 25,864 hrs · 22,433 cycles

ON FLIGHT 4512 THE CREW REPORTED THEY RECEIVED A HYD PUMP E1 FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED HYD NR 1 AS PER AMM 12-13-01. CHECK FOR LEAKAGE PER AMM 29-10-00. NO LEAKS NOTED. CHECK EMDP NR 1 FOR LEAKS AS PER AMM 29-10-00. CHECK EDP NR 1 PER AMM 29-10 -03. ALL OPERATIONAL CHECKS GOOD. NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,532 hrs · 22,195 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,892 hrs · 21,700 cycles

DURING B INSPECTION FOUND THE GALLEY CEILING EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CEILING EMERGENCY LIGHT LAMP IAW EMB-135 AMM 33-50-09. THE OPERATINOAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 24,752 hrs · 21,590 cycles

FLIGHT 4411, THE CREW REPORTED THE AFT CABIN FLASHLIGHT WAS INOPERATIVE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY PER SMP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 24,263 hrs · 21,207 cycles

THE CREW REPORTED A HEAVY FUEL SMELL IN COCKPIT AND CABIN ON START OF NR 2 ENGINE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED NORMAL ENGINE START/SHUTDOWN IAW AMM 71-00-00 NO DEFECTS NOTED. RAN THE AIRCRAFT FOR A LONG PERIOD OF TIME IN VARIOUS ENGINE BLEED AND AIR CIRCULATION MACHINE CONFIGURATIONS. NO SMELL NOTED REF EMB MM 21-20-00 AND 71-00-00 AND ETN EM-72-034. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM PANEL — MISSING (EXIT SIGN) · airframe 23,853 hrs · 20,903 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EXIT UPPER SIGN FORWARD TRIM MISSING RE-ENTRY NEF 25-20A. INSTALLED SIGN FORWARD TRIM IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,736 hrs · 20,813 cycles

DURING MAINTENANCE INSPECTION FOUND LEFT INTERIOR SIDEWALL EMERGENCY LIGHT INOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER NR 4 IAW EMB 135 AMM 33-50-11. OPERATIONAL WAS CHECK GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 23,680 hrs · 20,776 cycles

FLIGHT 4554, CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO CLOSE. AIRCRAFT REMOVED FROM SERVICE. CLEANED AND LUBRICATED MAIN CABIN DOOR IAW AMM 52-18-00. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,660 hrs · 20,761 cycles

DURING B-INSPECTION, FOUND THE RIGHT FORWARD WING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT FORWARD WING EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-00. THE OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,660 hrs · 20,761 cycles

DURING B-INSPECTION, FOUND THE LEFT WALL EMERGENCY LIGHT AFT OF WING EXIT DOOR IS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WALL EMERGENCY LIGHT AFT OF WING EXIT DOOR IAW AMM 33-50-13. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — DETACHED (MAIN DOOR) · airframe 23,495 hrs · 20,635 cycles

ON FLIGHT 4526 THE CREW REPORTED THE MAIN DOOR HANDLE CAME OFF DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-INSTALLED MAIN DOOR HANDLE IAW EMB-52-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 23,478 hrs · 20,621 cycles

ON FLIGHT 4455 THE CREW REPORTED THEY WERE UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE. (GATE AGENT WAS ABLE TO OPEN IT FROM OUTSIDE). THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE INTERNAL HANDLE LOOSE. RE-SECURED THE MAIN PASSENGER DOOR INTERNAL HANDLE IAW EMB AMM 52-18-05. ALL CHECKS WERE NORMAL. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,318 hrs · 20,502 cycles

SEAT 9A EMERGENCY EXIT SIGN INOP. PERFORMED OPC ON SEAT 9A EMERGENCY EXIT SIGN IAW AMM33-50-14 OPC GOOD AT THIS TIME.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,352 hrs · 20,451 cycles

DURING MAINTENANCE VISIT FOUND THE LEFT EMERGENCY EXIT VERTICAL SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY EXIT VERTICAL SIGN IAW AMM 33-50-14. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,499 hrs · 19,867 cycles

AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BULB, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,163 hrs · 18,676 cycles

DURING MAINTENANCE BASE CHECK FOUND THE RIGHT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,952 hrs · 18,491 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CABIN OVERHEAD PANEL INNER EXIT LOCATOR SIGN AND EXIT MARKING SIGN BESIDE LEFT EMERGENCY EXIT DOOR TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 5 INVERTER IAW EMB-135 AMM CHAPTER 33-50-11. THE OPERATIONAL CHECK WAS GOOD, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,826 hrs · 18,380 cycles

DURING MAINTENANCE BASE CHECK FOUND THE EMERGENCY LIGHTS AT SEAT 9A TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER NR 3 IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 33-50-00. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 20,722 hrs · 18,287 cycles

ON FLIGHT 4436 DURING THE CLIMB THE CREW REPORTED THE LOSS OF PRESSURIZATION CLIMBING THROUGH FLIGHT LEVEL 250, CABIN ALT 14,500 FEET. ALL BUT 4 OXYGEN MASKS IN THE CABIN WERE DEPLOYED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO BNA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THIS AIRCRAFT WAS INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT TO ABI. REMOVED AND REPLACED THE DIGITAL CONTROLLER IAW EMB135 AMM 21-31-01. THE OPERATIONAL CHECK WAS GOOD. THE PASSENGER OXYGEN MASKS WERE CONTAMINATED WITH MOISTURE. REMOVED AND REPLACED OXYGEN MASKS AT 2A, 3A, 5A, 6A, 7A, 8A, 9A, 10A, 11A, 12A, 2 EA AT 13A, 3 EA AT 4BC, 5BC AND 9BC IAW EMB135 AMM 35-20-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,617 hrs · 18,190 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE MAIN CABIN DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP ASSEMBLY IAW EMB 135 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,256 hrs · 17,871 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EXIT SIGN WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY AND POWER SUPPLY IAW EMB-135 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — LOOSE (CABIN) · airframe 18,980 hrs · 16,736 cycles

DURING A PS1 CHECK THE AISLE AFT EMERGENCY EXIT LIGHT WORKED INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE AISLE AFT EMERGENCY EXIT LIGHT CONNECTION TO BE LOOSE. RECONNECTED THE WIRES IAW EMBRAER AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,195 hrs · 16,055 cycles

DISC - DURING HMBV INSPECTION FOUND LT OMEGA BEAM CORRODED AT FRAME 29. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AND REPAIRED IAW EMB SRM 53-00-10 FIGURE 202 SHEET 2. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE EXACT CAUSE OF DAMAGE. (K)

Part: SKIN — DENTED (FUSELAGE) · airframe 18,195 hrs · 16,055 cycles

DISC - DURING HMBV INSP A DENT WAS DISCOVERED ON THE RT FUSELAGE SKIN BETWEEN FR 22 AND FR 23 AND BETWEEN STRINGERS 13R AND 15R. AIRCRAFT REMOVED FROM SERVICE. DAMAGE WAS REPAIRED IAW EMB SRM 53-21-01, 51-75-04 AND 51-10-03. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,195 hrs · 16,055 cycles

DISC - DURING HMBV THE LT SIDE OF THE CENTER BEAM WAS FOUND CORRODED AT THE THIRD CARBON CROSS BEAM FROM THE FRONT. AIRCRAFT REMOVED FROM SERVICE. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PIECES IAW EMB SRM 43-00-10 FIGURE 203. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,183 hrs · 16,044 cycles

DURING OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM AEAI WORKCARD 33-700-12 FOUND EXIT MARKER SIGNS AFT OF BOTH EMERGENCY EXITS TO BE INSTALLED IN THE WRONG POSITIONS AS ARROWS WERE NOT POINTING TOWARDS EMERGENCY EXITS. AIRCRAFT REMOVED FROM SERVICE. REPOSITIONED BOTH EMERGENCY EXIT MARKER SIGNS TO PROPER POSITION. PERFORMED OPERATIONAL CHECKS IAW AMM 33-50-14. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION, THE LT SIDE OF THE CTR BEAM WAS FOUND TO BE CORRODED AT THE THIRD CARBON CROSSBEAM FROM THE FRONT. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE EXACT CAUSE OF DAMAGE. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 24 TO FRAME 36. REMOVED AND REPLACED SEAT IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.

Part: CAP — CORRODED (LT MLG) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND LT MLG BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW AMM 32-10-01. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND SEAT TRACK FROM FRAME 36 TO FRAME 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND RIGHT SEAT TRACK BETWEEN FRAME 24 TO FRAME 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND GUSSET OVER CENTER HAT BEAM BETWEEN FRAME 18 TO FRAME 22 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND RIGHT INBOARD SEAT TRACK FROM FRAME 36 TO FRAME 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 56-10-01. RETURNED AIRCRAFT TO SERVICE.

Part: CAP — CORRODED (RT MLG) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND RIGHT MAIN LANDING GEAR BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-10-01. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (CORRODED) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND UPPER FLOORBEAM AT FRAME 22 BETWEEN SERVICE DOOR AFT SILL AND CENTER HAT BEAM CORRODED. REMOVED AND REPLACED FLOORBEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: CAP — CORRODED (RT MLG) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND RIGHT MAIN LANDING GEAR BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-10-01. RETURNED AIRCRAFT TO SERVICE.

Part: CAP — CORRODED (LT MLG) · corrosion level 2 · airframe 13,518 hrs · 12,205 cycles

FOUND LEFT MAIN LANDING GEAR BEARING CAP CORRODED. REMOVED AND REPLACED GEAR CAP IAW EMB AMM 32-10-01. RETURNED AIRCRAFT TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN LIGHTS)

DISC FLOOR PROXIMITY LIGHTS COME ON BY THEMSELVES AND WOULD NOT EXTINGUISH. REPLACED NR 3 BATTERY CHARGER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: STRINGER — CHAFED (FUSELAGE) · airframe 8,608 hrs · 8,062 cycles

DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT BELLEY FAIRING CUTOUT. BLENDED THE CHAFED AREA. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501981) (K)

Part: STRINGER — CHAFED (FUSELAGE) · airframe 8,608 hrs · 8,062 cycles

DURING AN IMBV INSPECTION STRINGER 19R WAS FOUND TO BE CHAFED AT AFT BELLY FAIRING CUT OUT. BLENDED THE CHAFED AREA. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DOEN IAW SRM. (SW21200501981) (K)

Part: CONTROL UNIT — FAILED (E/E BAY) · airframe 8,590 hrs · 8,050 cycles

DUAL PITCH TRIM FAIL ON CLIMBOUT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501813) (K)

Part: HYDRAULIC SYSTEM — FAILED (NR 1)

JFK - FLT 4775 - CREW REPORTED A HYDRAULIC SYSTEM 1 FAIL AFTER TAKEOFF. AIR TRAFFIC CONTROL DECLARED A PRECAUTIONARY EMERGENCY. CREW LANDED WITH NO FURTHER INCIDENTS REPORTED. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - AIRCRAFT ARRIVED FOR A MAIN BASE VISIT AND PERMENANT REPAIR OF TDMI NR 7395300A4 TWO DENTS BETWEEN FRAME 67 AND 68 IN AFT SECTION UNDER CARGO AREA. PERFORMED A CUT OUT OF THE DAMAGE AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB SRM (EMB-145/1142 REV 19) CHAPTER 53-31-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20. CUT OUT SECTION OF DAMAGED OMEGA BEAM AND APPLIED SURFACE TREATMENT. FABRICATED A FILLER, TWO SHIMS, BACK PLATE AND DOUBLER. REPAIR DONE IAW EMB SRM (EMB 145/1142 REV 19) 53-21-10 FIG 201 AND STANDARD SRM PROCEDURES. (M)