N710TB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
66 reports on file, 2000-08-26 – 2007-06-09.
Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 16,054 hrs · 14,574 cycles
STRONG OILY ODOR WITH ENGINE BLEEDS ON. REMOVED AND REPLACED NR 1 CARBON SEAL IAW ROLLS ROYCE MM 72-25-25. LEAK AND OPERATIONAL CHECKS GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
FORWARD CABIN FLOOR SILL LEFT SIDE CORRODED. REMOVED AND REPLACED LEFT FORWARD CABIN SILL IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
RIGHT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 36 AND 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 15,925 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 24 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
FORWARD CABIN FLOOR U-SHAPE AT FRAME 17 AND STRINGER 16 LEFT SIDE CORRODED. REMOVED AND REPLACED BRACKET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
FORWARD CABIN FLOOR SILL LEFT SIDE CORRODED. REMOVED AND REPLACED FLOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN 53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAME 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
FOUND FORWARD CABIN FLOOR SUPPORT AT FRAME 20 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 24 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN 53-110R2.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
RIGHT INBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM 53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,956 hrs · 14,467 cycles
FORWARD FLOOR SUPPORT AT FRAME 20 FOUND CORRODED. REMOVED AND REPLACED FLOOR SUPPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM 53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
UPPER FLOORBEAM AT FRAME 22 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
RIGHT INBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 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 15,925 hrs · 14,467 cycles
FOUND LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT INBOARD SEAT TRACK BETWEEN FRAME 17 AND 23 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 15,925 hrs · 14,467 cycles
RIGHT AFT INBOARD SEAT TRACK BETWEEN FRAMES 53 AND 57 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
FOUND FLOORBEAM AT FRAME 22 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,956 hrs · 14,467 cycles
RIGHT AFT INBOARD SEAT TRACK BETWEEN FRAME 53 AND 57 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
DURING MBV INSPECTION, FOUND FORWARD CABIN FLOOR U SHAPE BRACKET AT FRAME 17 AND STRINGER 16 LEFT SIDE CORRODED. REMOVED AND REPLACED BRACKET IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,925 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,926 hrs · 14,467 cycles
LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 15,743 hrs · 14,316 cycles
STRONG FUEL ODOR NOTICED WITH BOTH PACKS RUNNING, APU WAS ONLY BLEED SOURCE ON. RAN BOTH ENGINES WITH PACKS AND NO ODOR NOTED, MEL 49-01.
Earlier reports · 2000–2006 · 22 reports
2006
Part: WARNING SYSTEM — ACTIVATED (COCKPIT)
LGA - FLT 4844 - BLUE ADVISORY MESSAGE E1 HYDRAULIC PUMP FAIL. FOLLOWED AIRCRAFT OPERATING MANUAL AND TURNED ON NR 1 ELECTRIC HYDRAULIC PUMP. NR 1 ELECTRICAL HYDRAULIC PUMP. NR 1 HYDRAULIC SYSTEM FAIL ILLUMINATED AND NR 1 ELECTRIC HYDRAULIC PUMP WAS TURNED OFF. TURNED ON NR 1 ELECTRIC HYDRAULIC PUMP DURING APPROACH. SYSTEM PRESSURE RESTORED, E1 HYDRAULIC PUMP FAIL MESSAGE EXTINGUISHED. AFTER LANDING LOST NR 1 HYDRAULIC SYSTEM PRESSURE. LOST NOSE WHEEL STEERING WHEN NOSE LANDING GEAR TOUCHED DOWN. (M)
2005
Part: FLOOR SUPPORT — CORRODED (GALLEY)
A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A PLATE, FILLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M)
Part: FLOOR SUPPORT — CORRODED (FS 25)
A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. ADDITIONAL CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT THE GRAPHITE CROSSBEAM. REMOVED THE PREVIOUS REPAIR AND ENLARGED THE CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30 CHAPTERS 53-00-10. (M)
Part: FLOOR SUPPORT — CORRODED (FS 25)
THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M)
Part: FLOOR SUPPORT — CORRODED (GALLEY)
THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER. REPAIR DONE IAW EMB REPAIR IC2005-145/4212 DATED AUGUST 10, 2005. (M)
Part: SILL — CORRODED (SERVICE DOOR)
THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED A NEW SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02, 51-20-03, 51-40-06. (M)
2004
Part: ACTUATOR — INOPERATIVE (RUDDER) · airframe 10,528 hrs · 9,877 cycles
CREW REPORTED DURING CLIMB, THE RUDDER TRIM JAMMED RT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE YAW TRIM ACTUATOR IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.
Part: ECU — INOPERATIVE (MLG)
CREW REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE FOUND FIVE FAULTS LOADED IN THE CENTRAL MAINTENANCE COMPUTER. THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2003
Part: SILL — CORRODED (CARGO DOOR)
DURING AN IMBV INSPECTION, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 65-67. REMOVED EXISTING SILL. CLEANED AND TREATED THE AREA. INSTALLED NEW SILL IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-40-02 AND 51-20-03. (M)
2001
Part: SILL — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. REPAIRED CORRODED SERVICE DOOR FORWARD SILL IAW EMB 135 REPAIR STATEMENT GST-3128/01. (M)
Part: STRUCTURE — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, FOUND FORWARD INBOARD RIGHT CROSS MEMBER AT FRAME 22 CORRODED. INSTALLED NEW CROSS MEMBER IAW EMB 135 SRM. (M)
Part: GUSSET — CORRODED (FUSELAGE)
ABI - DURING MBV - INSPECTION, FOUND SERVICE DOOR FORWARD AND AFT GUSSET PLATES CORRODED. REMOVED AND REPLACED FORWARD AND AFT GUSSET PLATES IAW EMB 135 SRM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, CENTER FLOORBEAM BETWEEN FRAMES 24 AND 26 WAS FOUND TO BE CORRODED. REMOVED CORROSION IAW EMB 135 SRM 51-10-02. INSTALLED REPAIR DOUBLER ON CENTER FLOORBEAM IAW EMB 135 SERVICE LETTER GST 3143/01. (M)
Part: CAP — CORRODED (LT & RT MLG)
ABI - LEFT AND RIGHT MLG FORWARD AND AFT BEARING CAPS CORRODED. REMOVED AND REPLACED BEARING CAPS IAW EMB AMM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT FLOORBEAM AT FRAME 20. FABRICATED FILLER AND DOUBLER AND INSTALLED ON AIRCRAFT IAW EMB 135 SRM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING MBV RIGHT FLOORBEAM WAS TO BE CORRODED BETWEEN FRAMES 17 AND 18. REMOVED CORROSION IAW EMB 135 SRM 51-10-02. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING MBV, LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 AND 24. REMOVED CORROSION IAW EMB 135 SRM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING MBV, FOUND FORWARD DIGITAL TO BE CORRODED. REMOVED CORROSION AND FOUND TO BE ACCEPTABLE IAW EMB135 SERVICE LETTER GST 3128/01. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, FOUND CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 CORRODED. FABRICATED REPAIR DOUBLER AND INSTALLED ON AIRCRAFT IAW EMB 135 REPAIR STATEMENT GST-2930/01 AND EMB 135 SRM. (M)
Part: SILL — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, RIGHT SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 25 AND 31. REMOVED CORROSION IAW EMB135 SRM. (M)
Part: SILL — CORRODED (FUSELAGE)
ABI - DURING MBV, FOUND SERVICE DOOR AFT SILL CORRODED. INSTALLED REPAIR DOUBLER ON SERVICE DOOR AFT SILL IAW EMB 135 SERVICE LETTER GST 3128/01. (M)
2000
Part: TRIM MOTOR — MALFUNCTIONED (PITCH)
BOS - FLT 4874 - DURING CLIMB-OUT, CREW NOTED PITCH TRIM 2 FAIL, THEN SYSTEM 1 FAILED AND BACK UP. CREW RETURNED TO BOS. JUST AFTER LANDING PITCH TRIM SYSTEM OPERATED NORMAL. MAINTENANCE PERFORMED OPERATIONAL CHECK IAW EMB MM AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. (M)