N47202
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.
79 reports on file, 1998-08-13 – 2009-07-28.
Part: DOOR — STUCK (PAX DOOR) · airframe 26,593 hrs · 22,548 cycles
ASH FLT 7012 ALB TO ORD. PASSENGER DOOR WILL NOT OPEN. CONTRACT MX PERFORMED OPS CHECKS. NO DEFECTS NOTED.
Part: DOOR — STUCK (PAX DOOR) · airframe 26,582 hrs · 22,538 cycles
ASH FLT 7023 ORD-BHM. CREW REPORTED THAT THE PAX DOOR WILL NOT OPEN FROM EITHER THE INNER OR OUTER HANDLE. CONTRACT MX OPS CHECK GOOD.
Part: COMBUSTION LINER — DAMAGED (NR 2 ENGINE) · airframe 25,999 hrs · 21,958 cycles
COMBUSTION LINER DAMAGE NR 2 ENGINE. MX REPLACED COMBUSTION LINER.
Part: STRUT — LOW (MLG) · airframe 25,670 hrs · 21,610 cycles
ASH FLT 7193 IAD-LGA. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A LOUD BANG DURING LANDING GEAR RETRACTION. MX SERVICED ALL GEAR STRUTS.
Earlier reports · 1998–2008 · 75 reports
2008
Part: SEAL — DAMAGED (PAX DOOR) · airframe 24,871 hrs · 20,781 cycles
ASH FLT 7295 FWA-ORD. PASSENGER DOOR SQUEAL ENTIRE FLIGHT, NO PAX DOOR MESSAGES OR PRESSURIZATION DISCREPANCIES. MX REPAIRED DOOR SEAL.
Part: LIGHT — INTERMITTENT (CABIN)
AIRSHUTTLE 7173 IN ORD REPORTED THE EXIT LIGHT ON THE SERVICE DOOR INOPERATIVE. MAINTENANCE RESET THE SYSTEM AND WERE UNABLE TO DUPLICATE THE PROBLEM. (S)
Part: HANDLE — STIFF (PAX DOOR)
DIFFICULTY OPENING THE PAX DOOR. MX UNABLE TO DUPLICATE PROBLEM--OPS GOOD. (B)
Part: TILLER — OUT OF ADJUST (NLG STEERING) · airframe 23,970 hrs · 19,846 cycles
ASH FLT 7245 ORD-TVC - NOSE WHEEL STEERING INOP MESSAGE IN FLIGHT, PILOT DECLARED EMERGENCY. CENTERED TILLER, OPS GOOD.
Part: SPRING — BROKEN (F/A SEAT) · airframe 23,869 hrs · 19,745 cycles
ASH FLT 7230 ORD - CAE FORWARD FLIGHT ATTENDANT SEAT RETRACT SPRING BROKE. REMOVED AND REPLACED OUTBOARD SPRING, OPS NORMAL.
2007
Part: LINE — LEAKING (HYD SYSTEM) · airframe 23,304 hrs · 19,179 cycles
ASH FLT 7371 LGA- IAD- LOSING ALL HYD 3 FLUID WHILE TRYING TO EXTEND THE GEAR. REMOVED AND REPLACED HYDRAULIC LINE.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,155 hrs · 19,026 cycles
FLT 7484, PHL - EMERGENCY LIGHTS INOP, SWITCH LEFT ON. CHARGED EMERGENCY BATTERIES, OPS GOOD.
Part: BUTTON — STICKING (OXYGEN MASK) · airframe 22,884 hrs · 18,754 cycles
ASH FLT 7364- ORD-GSP - CAPTAIN'S O2 MASK PRESS TO TEST BUTTON WAS STICKING. MX CLEANED THE O2 MASK AND BUTTON.
Part: BRACKET — OUT OF ADJUST (EMERGENCY EXIT) · airframe 22,760 hrs · 18,817 cycles
ASH FLT 7192 IAD. LEFT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. ADJUSTED DOOR SENSOR BRACKET. OPS CHECK GOOD.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,538 hrs · 18,398 cycles
ASH 7188 ORD - EMERGENCY LIGHT AT ROW 2 INOP. MX RELAMPED AND OP CHECKED GOOD.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,366 hrs · 18,208 cycles
FS 310 HAS DAMAGE ON PREVIOUS SKIN REPAIR. PERFORMED A PERMANENT REPAIR TO FUSELAGE SKIN FS 310 STR 16-17.
Part: SKIN — DENTED (FUSELAGE) · airframe 22,366 hrs · 18,208 cycles
TWO DENTS LOCATED ON THE FUSELAGE SKIN AT FS 58.50% AND FS 64.50% BETWEEN STRINGERS 26L AND 26R DENTED. REPAIRED BY REMOVING DAMAGE, FABRICATING AND INSTALLING NON-FLUSH DOUBLER IAW.
Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 21,836 hrs · 17,714 cycles
ASH 7202 IAD - REPORTED STAB CHANNEL NR 1 W/ NOT ENGAGE. MX REMOVED AND REINSTALLED THE HSTCU, AND COULD NOT DUPLICATE THE PROBLEM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,398 hrs · 17,304 cycles
ASH 7320 IAD. PILOT REPORTED CEILING LEVEL EMERGENCY FLOOD LIGHTS AT ROW 5 INOP. MX RELAMPED FLOOD LIGHTS.
2006
Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 21,080 hrs · 16,921 cycles
ASH 7168 GSP. PILOT REPORTED AN OUTBOARD & INBOARD GROUND SPOILER FAULT MESSAGES. MX PERFORMED A RESET WITH CREW.
Part: CONTROL ROD — OUT OF ADJUST (THROTTLE) · airframe 20,879 hrs · 16,811 cycles
ASH 7257 MHT. PILOT REPORTED THAT THE RT ENGINE OIL PRESSURE DROPPED TO 10 PSI. FOLLOWED BY A IN FLT SHUTDOWN. MX ADJUSTED THROTTLE CONTROL ROD.
Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 20,871 hrs · 16,803 cycles
ASH 7199 CAK. OUTBOARD GND SPOILER FAULT. MX CONTROL RESET THE SYSTEM WITH THE CREW AND OP CHECKS WERE GOOD.
Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 20,599 hrs · 16,547 cycles
ASH 7302 IAD - CREW RTG DUE TO YAW DAMP NR 2 MESSAGE. MX REMOVED AND REPLACED NR 2 FCC CARD. OP'S CHECK GOOD.
Part: IDG — UNDERSERVICED (NR 1) · airframe 20,580 hrs · 16,523 cycles
ASH 7302 JFK - A/C ABORTED TAKEOFF AND RTG DUE TO NR 1 IDG CAUTION MESSAGE. MX SERVICED IDG.
Part: DOOR — DAMAGED (LT OVERWING) · airframe 20,561 hrs · 16,504 cycles
ASH 7101 CLT. LT OVERWING EMERGENCY EXIT DOOR DAMAGED. MX REPLACED DOOR.
Part: ELT — MALFUNCTIONED (CABIN) · airframe 20,554 hrs · 16,498 cycles
ASH 7101 CLT - ELT "ON" MASTER CAUTION WITH ELT TRANSMITTING UNCOMMANDED. MX REPLACED THE ELT.
Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 20,501 hrs · 16,446 cycles
ASH 7129 ORD - CAPTAIN REPORTED PAX DOOR HARD TO OPEN. MX OPERATED DOOR FOUND NO DEFECTS. DOOR OPERATED NORMALLY.
Part: CONTROL PANEL — MALFUNCTIONED · airframe 20,439 hrs · 16,388 cycles
ASH 7175 IAD. YAW DAMP 2 DISENGAGED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED YAW DAMP PANEL. OPS CHECK GOOD.
Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 20,342 hrs · 16,283 cycles
ASH 7188 ORD - STAB CHANNEL 1 INOP AND FLT SPOILER FAULT MESSAGE. MX RESET SYSTEM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,326 hrs · 16,268 cycles
ASH 7116 MLI. RIGHT REAR EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,198 hrs · 16,134 cycles
ASH 7366 IAD - CABIN NR 2 CEILING EMERGENCY LIGHT WAS INOP. MX REPLACED THE LAMP. OP'S CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,971 hrs · 15,845 cycles
ASH 7310 IAD. ROW 5 EMERGENCY LIGHT INOPERATIVE. MX RELAMPED.
Part: SPOILER — FAULTY (SPOILER SYS) · airframe 19,968 hrs · 18,843 cycles
ASH 7318 JFK. OB GROUND SPOILER FAULT. RESET SYSTEM AND FAULT CLEARED.
Part: TRIM SYSTEM — MALFUNCTIONED · airframe 19,909 hrs · 15,834 cycles
ASH 7352 CAK - STAB TRIM AND MACH TRIM WON'T ENGAGE. RESET SYSTEM.
Part: PRESSURE SWITCH — DIRTY (PAX DOOR) · airframe 19,769 hrs · 15,699 cycles
ASH 7010 CLT. PASS DOOR CAUTION IN FLIGHT. MX CLEANED PRESSURE SWITCH. (5-1-06)
Part: STRIP — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,739 hrs · 15,676 cycles
ASH 7218 ORD. LEFT HAND EMERGENCY EXIT DOOR CAUTION. MAINTENANCE ADJUSTED STRIP.
Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 19,739 hrs · 15,676 cycles
ASH 7218 ORD. PAX DOOR LATCH CAUTION. MAINTENANCE ADJUSTED PROX SWITCH. (4-28-06)
Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,732 hrs · 15,669 cycles
ASH 7107 IAD. LT OVER WING EMERGENCY EXIT CAUTION MESSAGE. MX CLEANED AND ADJUSTED PROXIMITY SWITCH AND OP'S CHECK NORMAL.
Part: DETECTOR — OUT OF ADJUST (TE FLAPS) · airframe 19,282 hrs · 15,228 cycles
WHILE MOVING THE FLAPS DURING THE CREWS PREFLIGHT INSPECTION, A FLAP FAIL CAUTION MESSAGE APPEARED. MX ADJUSTED FLAP SKEW DETECTOR. PART "A" INSP COMPLETED.
2005
Part: PRIORITY VALVE — FAULTY (NLG) · airframe 18,901 hrs · 14,819 cycles
ASH 7178 CLT - GEAR DISAGREE. NOSE INDICATION SHOWED RED. MX REMOVED AND REPLACED PRIORITY VALVE, PSEU PROX SENSOR, UPLOCK ASSEMBLY AND SERVICED STRUT.
Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 18,883 hrs · 14,801 cycles
ASH 7244 PHL - GEAR DISAGREE ON LANDING. MAINTENANCE RAN THE GEAR THROUGH SEVERAL TIMES AND NO FAILURE. TEST FLIGHT WAS GOOD.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,855 hrs · 14,771 cycles
ASH 7268 ORD - FLAPS FAILED AT 0 DEGREES. MAINTENANCE C/W PART A AND COULD NOT DUPLICATE THE DISCREPANCY
Part: ACTUATOR — FAILED (TE FLAPS) · airframe 18,855 hrs · 14,772 cycles
ASH 7014 BUF - FLAPS FAIL IN FLIGHT. MAINTENANCE REPLACED NR 3 AND NR 4 RT FLAP ACTUATOR.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,842 hrs · 14,759 cycles
ASH 7195 ORD - FLAPS FAIL AT 20 DEGREES. MAINTENANCE C/W PART B.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,842 hrs · 14,759 cycles
ASH 7199 ORD - FLAPS FAIL DURING DESCENT. FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES. MAINTENANCE C/W PART A.
Part: WARNING MESSAGE — ILLUMINATED · airframe 18,797 hrs · 14,708 cycles
ASH 7026 ORD, FLAP FAIL MESSAGE, FAIL AT 20 DEGREES. MAINTENANCE COMPLIED WITH PART A INSPECTION.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 18,797 hrs · 14,708 cycles
ASH 7010 ORD - FLAPS FAIL MASTER CAUTION. COMPLIED WITH PART A EARLIER AND PART B WAS COMPLIED WITH LATER. NO FURTHER DEFECT NOTED.
Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 18,754 hrs · 14,668 cycles
ASH 7247 ORD - FLAPS FAIL IN FLIGHT AT 4 DEGREES WHEN SELECTED TO 8 DEGREES ON EXTENSION. CONTRACT MAINTENANCE COMPLIED WITH PART A & B.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 18,757 hrs · 14,671 cycles
ASH 7206 FWA - FLAPS FAIL CAUTION IN FLIGHT AT 20 DEGREES. MAINTENANCE COMPLIED WITH PART B.
Part: CHECK VALVE — MALFUNCTIONED (NLG PRIORITY) · airframe 18,570 hrs · 14,497 cycles
ASH 2746 PIT - LANDING GEAR DISAGREE WARNING MESSAGE. REPLACED NOSE GEAR PRIORTY CHECK VALVE.
Part: COMPUTER — MALFUNCTIONED (FUEL QTY SYS) · airframe 17,011 hrs · 13,137 cycles
RETURNED TO FIELD DUE TO THE LT WING FUEL TANK QUANTITY INDICATION ERRATIC. MAINTENANCE WILL EITHER CHANGE THE FUEL COMPUTER OR COMPLY WITH MEL PROCEDURES. MAINTENANCE REMOVED AND REPLACED FUEL COMPUTER.
2004
Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 15,374 hrs · 11,684 cycles
ASH 2608 PHL. LAV SMOKE DETECTOR DID NOT ACTIVATE WITH PASSENGER CAUGHT SMOKING IN THE LAV. MX OPS CHECKED THE DETECTOR AND FOUND NO DEFECTS. NO PARTS USED.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,906 hrs · 11,299 cycles
CREW REPORTED RT SIDE EXTERIOR EMERGENCY LIGHT INOP. MX WAS CALLED. DURING THE RON MX REPLACED THE BULB.
2003
Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 14,264 hrs · 10,786 cycles
ASH 2690 SDF-PHL. DURING PREFLIGHT THE MAIN CABIN DOOR W/N OPEN NORMALLY WITH THE HANDLE FROM THE INSIDE. MX CLEANED AND LUBED THE DOOR. OP CHECKS GOOD. NO PARTS USED.
Part: ENGINE — DAMAGED (NR 2) · airframe 14,012 hrs · 10,591 cycles
ON DESCENT TO YOW PILOT FELT THE A/C SHUTTER. THE PILOT THAN NOTICED THE NR 2 ENGINE VIBS FOLLOWED BY HIGH ITT AND LOW OIL PRESSURE. AN IN-FLIGHT SHUTDOWN WAS INITIATED. AFTER AN UNEVENTFUL LANDING MX WAS CALLED. AFTER A BORESCOPE OF THE ENGINE IT WAS DETERMINED THAT THE ENGINE NEEDS TO BE REPLACED. MX IN THE PROCESS OF REPLACING THE ENGINE. ERTS 11/9/2003.
Part: WARNING LIGHT — ILLUMINATED (NLG)
RETURNED TO FIELD. GEAR DISAGREE WARNING MESSAGE ON TAKEOFF. MAINTENANCE TROUBLESHOT AIRCRAFT IAW AMM. NO DEFECTS NOTED. (M)
2002
Part: BATTERY — DISCHARGED (CABIN)
FLT 5805 - MKE-PHL - DURING MAINTENANCE CHECKS AFTER LANDING IN PHL MAINTENANCE NOTICED THE CENTER AISLE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE T-SHOT THE PROBLEM TO THE INVERTER. MAINTENANCE REMOVED AND REPLACED THE INVERTER. OP CHECKS GOOD. (M)
Part: PACKING — DAMAGED (NLG)
FLT 5853 - CLE-PHL - GEAR DISAGREE MESSAGE. NOSE GEAR WILL NOT RETRACT ON FIRST ATTEMPT. MAINTENANCE WAS CALLED. MAINTENANCE REPLACED PACKING, ADJUSTED TARGET. OP CHECKS GOOD IAW CRJ MM 32-21-00. (M)
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG)
FLT 5786 - CVG-CLT, DURING LANDING GEAR RETRACTION GOT GEAR DISAGREE MESSAGE. NOSE GEAR WAS SLOW TO RETRACT AND LOCK. AIRCRAFT LANDED WITHOUT INCIDENT IN CLT. MAINTENANCE ADJUSTED PROXIMITY SENSOR. OP CHECKS GOOD IAW CRJ AMM 32-35-05. (M)
Part: SELECTOR VALVE — INOPERATIVE (NLG W/W)
FLT 5887 - MKE-PHL, RETURNED TO FIELD WITH A GEAR DISAGREE MESSAGE WITH AN 'X' OVER THE NLG INDICATION ON THE PRIMARY PAGE. MAINTENANCE WAS CALLED, MAINTENANCE REMOVED AND REPLACED THE SELECTOR VALVE. OP CHECKS GOOD. (M)
2001
Part: FLAP — MALFUNCTIONED (WING)
FLT 5865 - SDF-PHL - INBOUND TO SDF, THE CREW HAD A FLAP FAIL CAUTION MESSAGE. THE MESSAGE APPEARED WITH THE FLAPS AT ZERO AND NOT SELECTED. MAINTENANCE PERFORMED PART A OF THE AD, RESET THE SYSTEM AND THERE WERE NO FURTHER MESSAGES OR DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE WHERE DURING OVERNIGHT IN PHL, PART B OF THE AD WAS COMPLIED WITH. (M)
Part: LIGHT — INOPERATIVE (EXTERIOR)
FLT 5753 - DURING PREFLIGHT, THE CREW NOTED THAT THE RIGHT WING FORWARD MOST EXTERNAL EMERGENCY FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE LATER REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHTS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M)
Part: CONNECTOR — DIRTY (CABIN)
DURING PREFLIGHT, THE PILOT REPORTED SEVERAL EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE CLEANED THE CONNECTORS ON THE TRACKS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
2000
Part: LATCH — BENT (PAX DOOR) · airframe 6,651 hrs · 5,058 cycles
LIT/CLT - FLT 5777 - ON DEPARTURE, PASSENGER DOOR WOULD NOT LOCK. PASSENGERS WERE DEPLANED AND THE DOOR LOCKED NORMALLY. THE AIRCRAFT WAS FERRIED TO PHL. MAINTENANCE FOUND THE DOOR HANDLE BENT. THE HANDLE WAS REPLACED, THE DOOR OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)
FLT 5840 - DCA-TYS - DURING PREFLIGHT, THE CREW NOTED THAT THE EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 2 THROUGH 5 WERE INOPERATIVE. THE AIRCRAFT RETURNED TO THE FIELD WHERE MAINTENANCE INSTALLED A NEW POWER INVERTER. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M)
Part: DOOR LATCH — MISRIGGED (PAX DOOR)
FLT 5750 - BHM-LIT - THE AIRCRAFT HAD AN AIRSTAIR DOOR THAT WOULD NOT OPEN IN BHM. AS THE AIRCRAFT WAS BEING PUSHED BACK THE FLIGHT ATTENDANT PULLED THE HANDLE TO LOCK THE DOOR AND HEARD A LOUD POP. THE PUSH BACK WAS STOPPED AND THEN THE CREW COULD NOT OPEN THE DOOR. MAINTENANCE BROUGHT THE AIRCRAFT BACK TO THE HANGAR AND FOUND THE INNER DOOR HANDLE CAM ROLLER TENSION NEEDED READJUSTED. MAINTENANCE RERIGGED THE CAM ROLLER, OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
1999
Part: LATCH — DIRTY (AIRSTAIR DOOR)
FLT 5771 - CLT-LIT - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE AIRSTAIR DOOR WOULD NOT LOCK. MAINTENANCE CLEANED AND LUBED THE UPPER LATCH ROLLER, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SOCKET — UNPLUGGED (CABIN)
PHL/CVG - FLT 5753 - THE CAPTAIN REPORTED THE EMERGENCY ESCAPE PATH LIGHT HAD A SMALL FORWARD SECTION INOPERABLE. MAINTENANCE FOUND THE PIN/SOCKET UNPLUGGED. MAINTENANCE REPLUGGED. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)
Part: MECHANISM — LACK OF LUBE (AIRSTAIR DOOR)
PHL/MKE - FLT 5809 - THE CAPTAIN REPORTED A STICKY AIRSTAIR DOOR. MAINTENANCE WAS SENT TO INVESTIGATE AND REPORTED NO DISCREPANCIES, LUBED THE DOOR. FUNCTION CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)
Part: BULB — FAILED (OVERWING)
DURING ROUTINE MAINTENANCE, FOUND THE LEFT FORWARD EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. THE BULB WAS REMOVED AND REPLACED, OPS CHECK GOOD. (M)
Part: BULB — FAILED (CABIN)
FLT 5757 - SWF-RDU - AFTER ARRIVAL IN RDU, THE CREW REPORTED THAT THE AFT CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BULBS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1998
Part: BRAKE — LEAKING (NR 1)
FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND THE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99ZZZX1522.
Part: BULB — FAILED (LT EMER EXIT)
FLT 5763 - STL-PHL - DURING PREFLIGHT INSPECTION, CREW NOTICED THAT THE AFT LEFT EMERGENCY EXIT OVERWING FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE CONTROL DEFERRED THE ITEM PER MEL 33-51-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M)
Part: BULB — FAILED (LT EMER EXIT)
FLT 5763 - STL-PHL - DURNG PREFLIGHT INSPECTION, CREW NOTICED THAT THE FORWARD LEFT EMERGENCY EXIT OVERWING FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE CONTROL DEFERRED THE ITEM PER MEL 33-51-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M)
Part: BULB — FAILED (ROW 2)
DCA\HSV - FLT 5792 - DURING POST WALK-AROUND, CAPTAIN FOUND THE CEILING EMERGENCY LIGHT AT ROW 2 WAS NOT ILLUMINATING. MAINTENANCE DEFERRED THE EMERGENCY LIGHT PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (X)
Part: BRAKE — LEAKING (NR 2)
FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND THE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99ZZZX1522.
Part: BRAKE — LEAKING (NR 3)
FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND THE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99ZZZX1522.
Part: BRAKE — LEAKING (NR 4)
FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND THE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99ZZZX1522.
Part: SEAL — DIRTY (PASSENGER DOOR)
CVG/PHL - FLT 5753 - CREW REPORTED CABIN DOOR WOULD NOT CLOSE. MAINTENANCE CLEANED AND LUBED DOOR SEAL, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)
Part: PSEU — MALFUNCTIONED (E/E BAY)
PHL/GHM - FLT 5760 - ON APPROACH TO BHM, THE LANDING GEAR WOULD NOT EXTEND. THE CREW MANUALLY EXTENDED THE GEAR. NO EMERGENCY WAS DECLARED, HOWEVER, THE TRUCKS WERE DISPATCHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SEVERAL GEAR RETRACTIONS, BUT COULD NOT DUPLICATE THE PROBLEM. THEY REMOVED AND REPLACED THE PSEU AS A PRECAUTIONARY MEASURE THEN TEST FLEW THE AIRCRAFT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)