N711PH
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.
89 reports on file, 2000-08-06 – 2013-08-25.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 29,671 hrs · 25,551 cycles
MAIN DOOR CABIN VERY HARD TO OPEN. CLEANED AND LUBRICATED MAIN DOOR CABIN DOOR ROLLERS IAW AMM 52-18-00. OPS CHECK GOOD.
Part: COVER — UNKNOWN (PAX DOOR) · airframe 29,669 hrs · 25,550 cycles
THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. R & R MAIN PAX DOOR INNER RELEASE HANDLE COVER IAW STANDARD MTX PRACTICES.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 29,523 hrs · 25,436 cycles
CREW RECEIVED EICAS FLAP FAIL MESSAGE PRIOR TO 10000' AND LESS THAN 250KTS DURING CLIMB OUT FLAPS INDICATED "0" DEGREES WHEN MESSAGE PRESENTED. THE CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A WAS R & R FLAP ELECTRONIC CONTROL UNIT IAW AE AMM 27-53-02, OPS CHECK IAW EMB 27-53-00, OPS CHECK GOOD. THE ACFT RETURN TO SERVICE.
Part: SWITCH — MISSING (FLASHLIGHT) · airframe 29,400 hrs · 25,341 cycles
DURING MX INSP, FOUND THE AFT CABIN EMERGENCY FLASHLIGHT MISSING ON/OFF SWITCH. THE ACFT WAS REMOVED FROM SERVICE. R & R THE AFT CABIN FLASHLIGHT IAW REQUIRED. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: DOOR — BINDING (MAIN CABIN) · airframe 29,311 hrs · 25,272 cycles
THE F/A REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED THE MAIN CABIN DOOR ROLLERS IAW AMM 52-18-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 28,982 hrs · 25,019 cycles
ON FLIGHT 4555 THE CREW REPORTED THAT AFTER GEAR LEVER WAS SELECTED THEY GOT A LANDING GEAR LEVER DISAGREE MESSAGE FOR ABOUT 30 SECONDS WITH AN AURAL WARNING, THEN THE MESSAGE WENT AWAY. THE GEAR SEEMED TO RETRACT SLOWER THAN NORMAL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EMB FIM TASK 32-32-00-810-803 STEP 5(1), (2), (9), (22) AND PERFORMED EXT/RET CHECK REF EMB AMM 32-30-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 28,978 hrs · 25,016 cycles
FLIGHT 4506. MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. PERFORMED ADJUSTMENT PAX DOOR, IAW AMM 52-18-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ROLLER — LACK OF LUBE (DOOR FRAME) · airframe 28,942 hrs · 24,994 cycles
ON FLIGHT 4411 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE WAS HARD TO OPERATE AND DID NOT SWING OPEN OR CLOSE EASILY. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 28,825 hrs · 24,906 cycles
ON FLIGHT 4526 THE CREW REPORTED THE FLIGHT ATTENDANT HAD A HARD TIME OPENING THE MAIN PASSENGER DOOR, IT WAS STICKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN CABIN DOOR. PERFORMED ADJUSTMENT TEST IAW EMB AMM 52-18-00. ALL CHECKS WITHIN LIMITS. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ELECTRONIC UNIT — FAULTY (LANDING GEAR) · airframe 28,737 hrs · 24,838 cycles
ON FLIGHT 4490 THE CREW REPORTED THAT ON CLIMBOUT, AFTER LANDING GEAR HANDLE SELECTED UP NOSE & RIGHT MAIN INDICATIONS WERE NORMAL AND SHOWING UP. LEFT MAIN INDICATION INITIALLY SHOWED HASH MARKS FOR 5-10 SECONDS AND THEN WENT RED FOLLOWED BY LG/LEVER DISAGREE WARNING ON EICAS. LEFT MAIN INDICATION NEVER SHOWED YELLOW IN TRANSIT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LGA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB MM 32-32-01. THE OPERATIONAL CHECK OF THIS LANDING GEAR EXTENSION AND RETRACTION CHECK WAS GOOD IAW EMB MM 32-30-00. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 28,598 hrs · 24,731 cycles
THE CREW REPORTED THEY RECEIVED A FLAPS FAIL EICAS MESSAGE. DECLARED AN EMERGENCY AND INITIATED 0 FLAP LANDING. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE FLAP ELECTRONIC CONTROL IAW AMM 27-53-02. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,558 hrs · 24,702 cycles
ON FLIGHT 4429 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR ROLLERS IAW EMB-135 AMM 20-30-02 STANDARD PRACTICES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 28,531 hrs · 24,684 cycles
DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR HARD TO OPEN BUT WITHIN LIMITS. NO TIME TO FIX. TDMI REMAINS OPEN. COMPLIED WITH DOOR HANDLE SUPPORT ASSEMBLY INSPECTION IAW ETN-EM-52-052. CONPLIED WITH MAIN DOOR LUBRICATION IAW EMB 52-18-00 OPS CHECK GOOD. PULL CHECK IS 40 LBS. TDMI ITEM CLOSED OUT. ALL WORK C/W IAW EMB 135 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — BINDING (MAIN PAX) · airframe 28,411 hrs · 24,590 cycles
DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR HARD TO OPEN. COMPLIED WITH DOOR HANDLE SUPPORT ASSY INSPECTION IAW ETN-EM-52-052. COMPLIED WITH MAIN DOOR LUBRICATION IAW 52-18-00, OPS CHECKED GOOD. PULL CHECK IS 40 LBS. WORKED IAW AMM 52-18-00. AIRCRAFT RETURNED TO SERVICE.
Part: BOLT — LOOSE (CABIN DOOR) · airframe 28,314 hrs · 24,512 cycles
ON FLIGHT 4498 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS TOO DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE BOLTS AT INT DOOR HANDLE BOX. TIGHTENED BOLTS AND LUBED DOOR ROLLERS AND SEALS. DOOR AT HIGH END OF LIMITS IAW EMB MM 53-21-02 AND 52-18-00. PERFORMED THE ADJUSTMENT OF THE PAX DOOR IAW EMB MM 52-18-00 TO REDUCE THE AVERAGE MAX LOAD OF THE INTERNAL HANDLE PULL TEST TO A VALUE OF LESS THAN 45LBS ON OR BEFORE 200FC. THE AIRCRAFT WAS RETURNED TO SERVICE.
Earlier reports · 2000–2012 · 74 reports
2012
Part: DOOR — DIRTY (CABIN) · airframe 27,931 hrs · 24,220 cycles
ON FLIGHT 4510 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED THE MAIN DOOR IAW EMB 135 AMM # 52-10-01/53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — DIRTY (CABNI) · airframe 27,844 hrs · 24,148 cycles
ON FLIGHT 4488 THE CREW REPORTED THE MAIN DOOR HANDLE WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR IAW EMB 135 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 27,083 hrs · 23,565 cycles
DURING MAINTENANCE INSPECTION, FOUND THE MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE AT LGA ARRIVAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS ON MAIN CABIN DOOR IAW AE CRJ STANDARD MAINTENANCE PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (ROW 13A TO 16A) · airframe 27,059 hrs · 23,546 cycles
DURING MAINTENANCE INSPECTION, FOUND THE FLOOR LIGHT STRIP FROM ROW 13A TO 16A INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP IAW MM 33-50-12 AND LAMP. THE OPS CHECKED GOOD IAW MM 33-50-00. AIRCRAFT RETURNED TO SERVICE.
Part: GUARD — CONTAMINATED (CABIN) · airframe 27,025 hrs · 23,521 cycles
ON FLIGHT 4448 THE CREW REPORTED THE LANDING GEAR EMERGENCY (FLOOR ACCESS) COMPARTMENT "GEAR DOORS" SAFETY GUARD (RED) WAS FROZEN WITH DIRT. UNABLE TO ACCESS "GEAR DOORS" TOGGLE SWITCH. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED AND CLEANED LANDING GEAR EMERGENCY FLOOR ACCESS PANEL.IAW EMB AMM 20-30-02. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM) · airframe 26,874 hrs · 23,405 cycles
ON FLIGHT 4535, THE CREW REPORTED THE PITCH TRIM MAIN WAS INOPERATIVE AFTER TAKEOFF. THE CREW ELECTED TO RETURN TO DEPARTURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STABALIZER CONTROL UNIT IAW EMB-135 AMM 27-40-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 26,869 hrs · 23,400 cycles
FLIGHT 4535, CREW REPORTED MAIN CABIN DOOR WAS VERY HARD TO OPEN AND CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED THE ROLLER AND PERFORMED THE DYNAMOMETER IAW EMB-145 AMM 52-18-00 IT IS WITHIN AVERAGE LOAD. NO FURTHER DAMAGE NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,761 hrs · 23,318 cycles
DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT ABOVE THE RIGHT WING INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,566 hrs · 23,165 cycles
DURING MAINTENANCE PS2 INSPECTION FOUND THE GALLEY EMERGENCY LIGHT LAMP FOUND INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT BULB IAW AMM 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — OUT OF ADJUST (PAX) · airframe 26,449 hrs · 23,074 cycles
DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR HARD TO OPEN. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED ROD VI OF PASSENGER DOOR AND PRESSURIZATION CHECK. ALL OPERATIONAL CHECKS AND GAP MEASUREMENTS GOOD. NRWC 711-CMH-00702. AIRCRAFT RETURNED TO SERVICE.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 26,344 hrs · 22,995 cycles
ON FLIGHT 4477 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR HANDLE WAS VERY DIFFICULT TO OPEN FROM INSIDE AND THEN THE DOOR STICKS AND IS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN PASSENGER DOOR. PERFORMED OPERATIONAL CHECK IAW MM 52-10-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SEAL — OBSTRUCTED (CABIN DOOR) · airframe 26,289 hrs · 22,947 cycles
DURING FLIGHT 4510 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEBRIS FROM DOOR SEAL IAW STANDARD MAINTENANCE PRACTICES. OPENED AND CLOSED MAIN CABIN DOOR IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,239 hrs · 22,910 cycles
DURING B-INSPECTION FOUND THE CENTER AISLE OVERHEAD AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 26,122 hrs · 22,829 cycles
ON FLIGHT 4431 THE FLIGHT ATTENDANT REPORED MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN CABIN DOOR IAW 52-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 26,087 hrs · 22,800 cycles
ON FLIGHT 4468 THE FLIGHT ATTENDANT REPORTED THE ENTRY DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED DOOR & PERFORMED AN OPERATIONAL CHECK PER EMB AMM 52-10-00. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR — OUT OF RIG (CABIN) · airframe 26,067 hrs · 22,785 cycles
ON FLIGHT 4555 THE CREW REPORTED THE MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED TURNOVER AND RIG OF MAIN PASSENGER DOOR REF EMB AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD AND PRESSURE CHECKED GOOD AT THIS TIME NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,825 hrs · 22,592 cycles
AFT OVERWING RT EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERHEAD RT EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07, OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,791 hrs · 22,565 cycles
EMERGENCY FLOOR LIGHTING STRIP INOP. REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IAW EMB AMM 33-50-12.
Part: NUT — LOOSE (CABIN DOOR) · airframe 25,530 hrs · 22,372 cycles
ON FLIGHT 3231 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND NUT LOOSE ON DOOR OPEN ROD LINKAGE, RE-SECURE NUT. THE DOOR OPERATIONAL CHECK WAS GOOD IAW EMB 135 52-10-00 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,498 hrs · 22,339 cycles
DURING MAINTENANCE INSPECTION FOUND THE MOST AFT AISLE LIGHT STRIP AND LEFT FORWARD EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERNAL EMERGENCY LEFT LIGHT IAW AMM REFERENCE 33-50-10. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP LIGHT IAW AMM REFERENCE 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 25,332 hrs · 22,203 cycles
ON FLIGHT 3250 THE CREW REPORTED THE MAIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF THE CABIN DOOR IAW 52-18-00, WITH NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ANGLE — CORRODED (VERTICAL STAB) · airframe 25,268 hrs · 22,145 cycles
DURING MAINTENANCE BASE VISIT FOUND FOUND VERTICAL STABILIZER HAS A LEFT UPPER TRAILING EDGE PROFILE ANGLE CRACKED AT LOWER END. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,268 hrs · 22,145 cycles
DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED AT CROSSMEMBER AT FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.
2010
Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,628 hrs · 16,863 cycles
DURING INSPECTION FOR FLIGHT 4515 MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP AT SEAT 2A TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 INVERTER IAW EMB-135 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 22,542 hrs · 19,783 cycles
DURING MAINTENANCE BASE VISIT FOUND THE NR 1 FLOOR PROXIMITY STRIP WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.
2009
Part: SKIN — DENTED (LEFT WING) · airframe 21,315 hrs · 18,723 cycles
DURING MAINTENANCE CHECK IN ABI, THE AIRCRAFT FELL OFF JACK DENTING WING. ENTERED TIME DEFERRED MAINTENANCE ITEM TO PERFORM PERMANENT REPAIR OF LEFT LOWER WING SKIN ON OR BEFORE 250 FLIGHT CYCLES IAW EO EM-5700-425 PART C. AIRCRAFT REMOVED FROM SERVICE. PERMANENT REPAIR SCHEME WRITTEN AND TRANSFERRED TO EO EM-57MR-441. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH EO EM-57MR-441. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,100 hrs · 18,528 cycles
DURING PREFLIGHT INSPECTION FOR FLIGHT 4723 FOUND THE FORWARD FLOOR EMERGENCY LIGHTING STRIP INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLOOR EMERGENCY LIGHT STRIP. AIRCRAFT RETURNED TO SERVICE.
Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 20,909 hrs · 12,355 cycles
ON FLIGHT 4855 - CREW REPORTED AT APPROXIMATELY 15 MINUTES AFTER DEPARTURE FROM LGA GOT "ENGINE 1 HYDRAULIC 1 PUMP FAIL" MSG ON EICAS. RAN APPROPRIATE PROCEDURES. ELECTRICAL HYDRAULIC PUMP CAME ON AND OPERATED NORMALLY. APPROXIMATELY 5 MINUTES LATER "ENGINE 1 HYDRAULIC PUMP FAIL" MESSAGE WENT AWAY AND ELECTRICAL HYDRAULIC 1 PUMP TURNED OFF. ALTHOUGH HYDRAULIC QUANTITY WAS LOW (GREEN RANGE) SYSTEM SEEMED TO OPERATE NORMALLY. SEVERAL MINUTES LATER "ENGINE 1 HYDRAULIC PUMP FAIL" MESSAGE RE-APPEARED AND STAYED ON. AGAIN ELECTRIC HYDRAULIC 1 PUMP TURNED ON, HYDRAULIC 1 QTY REMAINED LOW. AGAIN ELECTRICAL HYDRAULIC 1 PUMP TURNED ON, HYDRAULIC 1 QTY REMAINED LOW. CREW DECLARED AN EMERGENCY. EMERGENCY VEHICLES WERE STANDING BY, AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE ENGINE DRIVEN PUMP PRESSURE SWITCH, SYSTEM 1 HYDRAULIC ACCUMULATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,831 hrs · 18,283 cycles
DISC - DURING MBV INSPECTION FOUND LEFT OMEGA BEAM JUST FORWARD OF FRAME 34 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 34 IAW EMB SRM 53-00-10 ITEM 3A-K. AIRCRAFT WAS RETURNED TO SERVICE.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,831 hrs · 18,283 cycles
DISC - DURING MBV INSPECTION, SERVICE DOOR AFT SILL WAS FOUND CORRODED AT FRAME 22. AIRCRAFT REMOVED FROM SERVICE. SERVICE DOOR SILL WAS REPLACED IAW SRM 51-20-03. AIRCRAFT WAS RETURNED TO SERVICE.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,831 hrs · 18,283 cycles
DISC - DURING MBV INSPECTION FOUND SERVICE DOOR CENTER SILL IS CORRODED AT FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.
Part: BALLAST — BURNED OUT (EMERGENCY LIGHTS)
ON FLIGHT 3739, ON GROUND CREW REPORTED A STRONG ODOR IN CABIN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BALLAST AND CONTROL. OPERATION CHECK GOOD, NO ODOR AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,328 hrs · 17,859 cycles
ON FLIGHT 4773 DURING PRE-FLIGHT CREW FOUND EMERGENCY AISLE LIGHT INOPERATIVE. ALL OTHER LIGHTS WORKING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED OVERHEAD EMERGENCY EGRESS BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PROXIMITY SENSOR — DAMAGED (SPOILER) · airframe 19,812 hrs · 17,443 cycles
ON FLIGHT 4758, CREW REPORTED SPOILER FAIL MESSAGE IN FLIGHT AND THEN HAD DAU 1 WARNING MISCOMP MESSAGE ON EICAS / DECLARED EMERGENCY AND DIVERTED TO. ACFT REMOVED FROM SERVICE. FOUND BROKEN PIN ON LT OTBD SPOILER PROXIMITY SENSOR. REMOVED AND REPLACED SENSOR IAW AMM 27-63-04 AND PERFORMED OPS CHECK IAW AMM 27-63-01. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.
2007
Part: LIGHT — UNKNOWN (CABIN) · airframe 16,370 hrs · 14,645 cycles
RECEIVED ELECTRIC EMERGENCY ABNORMAL AND EMERGENCY LIGHTS NOT ARMED MESSAGES, RETURNED TO DCA. REINITIALIZED ELECTRICAL SYSTEM IAW EMB AMM 24-36-00 WITH NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH ELECTRICAL LOAD TRANSFER NORMAL AND OPERATIONAL CHECK OF EMERGENCY LIGHTS WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,957 hrs · 14,288 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 15,957 hrs · 14,288 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: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,957 hrs · 14,288 cycles
Z PROFILE CORRODED AT FRAME 22. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,967 hrs · 14,288 cycles
CENTER OMEGA BEAM CORRODED ON INBOARD SIDE OF CROSSBEAM AT FRAME 32. REPAIRED OMEGA BEAM IAW EMB IC2007-145-0348 AND EMB SRM 53-10-03. AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,957 hrs · 14,288 cycles
RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 21 AND 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,957 hrs · 14,288 cycles
LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 53 AND 55. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,957 hrs · 14,288 cycles
LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 21 AND 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,967 hrs · 14,288 cycles
LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.
2006
Part: ENGINE — MALFUNCTIONED (NR 1)
OIL SMELL FROM PACKS DURING DESCENT. RAI NR 1 ENGINE, LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WARNING MESSAGE — ACTIVATED (WARNING SYS)
BAGG SMOKE EICAS WARN ABORTED TAKEOFF CARGO FIRE BOTTLE WAS BLOWN. REPLACED FIRE BOTTLES FOLLOWED WORK SCOPE AND FOUND NO DEFECTS. ALSO, REPLACED TEST SWITCH AS PRECAUTION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
2005
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)
THE CENTER FLOOR EMERGENCY LIGHT STRIPS WERE FAILED TO TEST. REPLACED THE DC/AC INVERTER ASSY. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)
Part: FLOOR SUPPORT — CORRODED (GALLEY)
THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4287 DATED AUGUST 11,2005. (M)
Part: FLOOR SUPPORT — CORRODED (GALLEY)
THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING TWO CUT OUTS. FABRICATED A REPAIR CHANNEL TO COVER BOTH CUTOUTS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4307 DATED AUGUST 12, 2005. (M)
Part: FLOOR SUPPORT — CORRODED (FS 20)
A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR. FABRICATED A DOUBLER, (EPNEM53EP54701) AND FILLER (EPNNEM53EP54703). FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02 AND 53-00-10. (M)
Part: INSULATION — INGESTED (FWD ELECT COMP)
BURNING PLASTIC SMELL REPORTED BY F/A IN CABIN DURING FLIGHT. NO SMOKE NOTED.. REMOVED THERMOCOUPLE INSULATION OUT OF BOTH FWD ELECTRONIC COMPARTMENT INTERNAL RECIRCULATION FANS. FUNCTIONAL CHECK FLIGHT PASSED. AIRCRAFT RETURNED TO SERVICE. (K)
Part: BATTERY PACK — DISCHARGED (CABIN)
BOS - FLT 4585 - CREW REPORTED AN EMERGENCY EXIT SIGN IN CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK POWER SUPPLY NR 5 IAW EMB 135 AMM 33-50-04. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2004
Part: BALLAST — INOPERATIVE (LAV LIGHT)
RDU - FLT 4624 - CREW REPORTED WHILE ON THE GROUND THE LAVATORY SMOKE DETECTOR WENT OFF WITHOUT ANY VISUAL INDICATION OF SMOKE. THERE WAS A STRONG BURNING ODOR IN LAVATORY. MAINTENANCE REMOVED AND REPLACED A BALLAST CONVERTER IN LABATORY IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
Part: STRINGER — CRACKED (FWD FUSELAGE)
AIRCRAFT STRUCK BY GPU ON RT SIDE JUST AFT OF RADOME. REPLACED 2 SKIN PANELS, 1 STRINGER, AND 1 FRAME. IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406972)
2003
Part: SKIN — GOUGED (FUSELAGE)
AIRCRAFT ARRIVED FOR PERMANENT REPAIR OF TDMI NR 71153018B, REPAIR OF BLENDED GOUGE BETWEEN STATION 66-67 AND BETWEEN STRINGERS 15-16R. PERFORMED EDDY CURRENT INSPECTION A POSITIVE CRACK INDICATION AS DETECTED. PERFORMED A CUTOUT OF THE DAMAGED AREA. AN ADDITIONAL NDT INSPECTIN WITH NO CRACK INDICATION NOTED. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, EMB SRM 145-1142 REV 22, CHAPTER 53-31-01. (M)
Part: LEVER — INOPERATIVE (TE FLAP)
DURING APPROACH CREW REPORTED THE FLAPS FAILED. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: ODOR — DETECTED (COCKPIT/CABIN)
PVD - FLT 4796 - DURING CRUISE FLIGHT, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT AND CABIN. CREW DECLARED AN EMERGENCY AND DIVERTED TO PVD. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS INSPECTED AND AN OPERATIONAL CHECK WITH ENGINES RUNNING WAS COMPLIED WITH. NO DEFECTS WERE NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
2002
Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY)
JFK - FLT 4748 - DURING FLIGHT CREW REPORTED E1 REVERSER DISAGREE AND SPOILER MESSAGE ON EICAS. AIRCRAFT DIVERTED TO JFK. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROLUNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2001
Part: SPRING — CORRODED (RT MLG) · corrosion level 2
THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT MLG UPLOCK SPRING CORRODED. REMOVED AND REPLACED UPLOCK SPRING IAW EMB135 AMM 32-33-10-000-801A AND 32-33-10-400-801A. (M)
Part: SPRING — CORRODED (LT MLG)
THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27613. LEFT MLG UPLOCK SPRING CORRODED. RAI SERVICEABLE LEFT MLG UPLOCK SPRING IAW EMB 135 AMM 32-33-10-000-801A AND 32-33-10-400-801. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING MBV INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A Z REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3598/01, PARA 3 AND STANDARD SRM PRACTICES. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 24. REMOVED CORROSION. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A Z REPAIR DOUBLER. REPAIR DONE IAW EMB GST 3598/01, PARA 8 AND STANDARD SRM PRACTICES. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING A MBV, FOUND CORROSION ON THE GALLEY CENTER OMEGA BEAM. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION ON THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A 'Z' REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3598/01 PARA 7 AND STANDARD SRM PRACTICES. (M)
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2
ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM CORRODED. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND EMB GST 2930/01. (M)
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2
ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT BEAM CORRODED AFT OF FORWARD CROSSBEAM. FABRICATED AND INSTALLED DOUBLER IAW EMB GST-3598/01. (M)
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2
THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY AREA RIGHT FORWARD SILL CORRODED. SILL REPAIRED IAW EMB GST 3598/01. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2
THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED LEFT OMEGA BEAM AT FRAME 20 IAW EMB 135, SRM 53-210 AND 51-40-02. (M)
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2
THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. LEFT SILL IN GALLEY ARM CORRODED. FABRICATED AND INSTALLED DOUBLER IAW EMB GST-3598/01. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE RIGHT OMEGA FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING. PERFORMED NDT INSPECTION ON THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A U REPAIR DOUBLER. REPAIR DONE IAW EMB GST-3598/01 PARA 6 AND STANDARD SRM PRACTICES. (M)
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2
ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. RIGHT BEAM AFT DIAMOND GUSSET CORRODED. INSTALLED SERVICEABLE RIGHT AFT DIAMOND IAW EMB 135 SRM 51-40-02. (M)
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2
ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27618. GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB 135 SRM 51-40-02. (M)
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2
ABI - THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. GALLEY CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED GALLEY CENTER BEAM GUSSET IAW EMB 135/145 SRM 51-40-02. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION. FABRICATED DOUBLER AND INSTALLED IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 15, 53-21-10, PAGE 201, FIG 201, SHEET 1 AND STANDARD SRM PRACTICES. (M)
2000
Part: CLAMP — BROKEN (NR 1 ENGINE)
PHL - FLT 4959 - DURING CLIMB-OUT, CREW HEARD A LOUD POPPING NOISE FOLLOWED BY PRESSURIZATION SPIKE. THERE AFTER CREW NOTED BLEED LEAK ON E1 WITH CARGO SMOKE DETECTOR ILLUMINATED. CREW BLEW BOTTLES AND DECLARED AN EMERGENCY AND RETURNED TO PHL. AIRCRAFT LANDED SAFELY AWAITED BY CFR. AFTER CFR INVESTIGATED NO EVIDENCE OF FIRE WAS DETECTED. NOTE PASSENGERS WAS DEPLANED NORMALLY AT THE GATE. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AND REPLACED CLAMP AND SEAL. OPS CHECK GOOD. (M)
Part: WARNING SYSTEM — FALSE ACTIVATION (NR 2 ENGINE)
DFW - FLT 3683 - DURING TAKEOFF ROLL, CREW NOTED ENG 2 LOW N1 DISPLAY ON EICAS. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE RE-ENTERED TAKEOFF DATA AND COMPLIED WITH GROUND ENGINE RUNS. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURND TO SERVICE. (M)