N971NA
Registered owner: NUWAY AG LLC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Executive Air Charter LLC (E5AA) | Operator | on 1990-11-26 | Operator named in NTSB report |
Accident & incident history
Operated by EXECUTIVE AIR CHARTER, INC. (per NTSB report)
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, 1995-07-03 – 2002-09-07.
Part: CONTROL CABLE — BROKEN (RUDDER)
DURING WORK TO CLEAR A MEL, UNDER CEILING PANEL OF GALLEY AREA, FOUND RUDDER CABLE WITH BROKEN STRAND. REMOVED AND REPLACED RUDDER CABLE ASSEMBLY LOCATED BETWEEN FRAME 38-47 AS PER MM 27-21-00. (M)
Part: SPAR — CORRODED (STABILIZER)
DURING MBV-1 INSPECTION, RIGHT HORIZONTAL STABILIZER AFT SPAR HAS AREA OF CORROSION. C/A: REPAIRED CORROSION IAW EO. AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, SEAT TRACKS, LEFT FORWARD OUTBOARD, LEFT FORWARD INBOARD, RIGHT FORWARD INBOARD, RIGHT FORWARD OUTBOARD, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MID INBOARD, WERE FOUND TO BE CORRODED. RAID SEAT TRACKS, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD, LEFT FORWARD OUTBOARD, RIGHT FORWARD OUTBOARD, LEFT MID OUTBOARD IAW E1.
Part: BULKHEAD — CORRODED (FRAME 1)
DURING MBV1 INSPECTION FOUND BONDING POINTS ON FORWARD BULKHEAD TO BE CORRODED. REPAIRED IAW ATR SRM. AIRCRAFT WAS RETURNED TO SERVICE.
Part: FRAME — CORRODED (FUSELAGE)
SAW - DURING CPCP2 INSPECTION, FOUND FRAME 37R CORRODED AT FLOOR LEVEL. REPAIRED CORRODED AREA IAW ATR SRM 53-67-70. (M)
Part: SEAT SPRING — CORRODED (CABIN)
DURING CPCP2 INSPECTION FOUND AFT CARGO WALL AND LEFT MIDDLE INBOARD SEAT TRACKS TO BE CORRODED.
Part: SILL — CORRODED (SILL PLATE)
DURING CPCP 2 INSPECTION FOUND SERVICE DOOR SILL PLATE CORRODED.
Part: FRAME — CORRODED (CABIN)
DURING CPCP 2 INSP FOUND FRAME 37R CORRODED AT FLOOR LEVEL.
Part: SKIN — DENTED (VERTICAL STAB)
DURING MBV 1 INSPECTION FOUND LEFT SIDE OF VERTICAL STABILIZER TO HAVE 2 DENTS.
Part: PAN — CRACKED (SERV DOOR PAN)
DURING MBV INSPECTION FOUND LOWER CORNER OF SERVICE DOOR PAN CRACKED.
Part: FRAME — CRACKED (FUSELAGE)
DURING MBV-1 INSPECTION, FRAME 25 LEFT AND RIGHT SIDES FOUND CRACKS IN LOWER OUTBOARD RADIUS OF HYDRAULIC LINE PASS THROUGH CUTOUTS.
Part: PANEL — CORRODED (WING)
DURING MBV-1 INSPECTION, RIGHT AILERON OUTBOARD UPPER PANEL CORRODED AROUND SCREW HOLES.
Earlier reports · 1995–2001 · 67 reports
2001
Part: WIRE — BROKEN (CABIN)
MIA - FLT 5248 - CREW REPORTED THE EMERGENCY EXIT SIGN AT THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: STRUCTURE — VIBRATION (FUSELAGE)
MIA - FLT 5369 - VERY STRONG VIBRATION NOTICED AFTER GEAR RETRACTION, MAX SPEED 160KIAS. RETURNED TO MIA. PERFORMED NOSE LANDING GEAR FORWARD DOOR PRELOAD CHECK AND GEAR EXTENSION AND RETRACTION IAW AMM. FOUND DOORS FLUSH AND IN CONTACT WITH STOPS. OPS CHECK GOOD. (M)
Part: SWITCH — INOPERATIVE (COCKPIT)
JAX - FLT 5248 - CREW REPORTED THE AILERON TRIM TO BE INOPERATIVE AT AN UNLEVEL POSITION. CAPTAIN NOTED IT TOOK ABOUT THIRTY POUNDS OF PRESSURE TO MAINTAIN LEVEL FLIGTH. MAINTENANCE REMOVED AND REPLACED THE TRIM CONTROL PANEL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: WARNING LIGHT — ILLUMINATED (COCKPIT)
FLL - FLT 5427 - CREW REPORTED AFTER TAKEOFF, AN ANTI-SKID FAULT ON RIGHT SIDE. FLIGHT DIVERTED TO MIA DUE TO WET RUNWAYS IN NAS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED OPS CHECK OF ANTI-SKID IAW AMM 32-42. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: PROPELLER — MALFUNCTIONED (NR 1 ENGINE)
MIA - FLT 5251 - AFTER TAKEOFF, CREW REPORTED THE NR 1 PROPELLER SPEED WENT TO ZERO. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BLADE (NR 1 PROP)
MIA - FLT 5257 - DURING CLIMB-OUT, CREW NOTICED UNUSUAL PROPELLER VIBRATION. REDUCING POWER ON NR 1 ENGINE REDUCED THE VIBRATION. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLADE ON THE NR 1 PROPELLER IAW ATR MM. OPS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
MCO - DURING PS CHECK MAINTENANCE FOUND FLOOR PROXIMITY LIGHTS AT 1AB, 3AB, AND 4AB TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THREE EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY PACKS (S/N'S 480, 26685, 17819). OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - FLT 5421 - CREW REPORTED FLOOR PROXIMITY LIGHTS IN THE FORWARD SECTION ARE INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE FOUND CANNON PLUG FOR THE POWER SUPPLY UNIT DIRTY. CANNON PLUG WAS CLEANED, OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2000
Part: DOOR — MISSING (FUSELAGE)
MCO - FLT 5277 - AIR CONDITIONING EXTERNAL CONNECTOR ACCESS DOOR CAME OFF IN FLIGHT, ENTERED INTO CDL. MAINTENANCE INSTALLED NEW DOOR IAW ATR MM. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT AFT INBOARD AND RIGHT AFT OUTBOARD CARGO SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3082. (M)
Part: FRAME — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FRAME 45 CORRODED. MAINTENANCE REMOVED AND REPLACED FRAME 45 FROM STRINGER 19L TO 20R IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3081. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT AFT INBOARD AND RIGHT AFT OUTBOARD CARGO SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SKIN — DENTED (FUSELAGE)
SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED A DENT IN THE FUSELAGE AT FRAME 17R BETWEEN FRAME 27A AND 28A. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SILL — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FRAME — MISDRILLED (FUSELAGE)
DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FRAME 35 MISDRILED BETWEEN STRINGERS 4L AND 5L. MAINTENANCE REPAIRED FRAME 35 IAW SRM 53-00-00 FIGURE 417. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED TWO SERVICE DOOR SILL PLATE INTERCOSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FITTING — CORRODED (TRUNNION)
SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT MLG UPPER TRUNNION SUPPORT CORRODED ON TOP INBOARD SIDE. MAINTENANCE BLENDED CORROSION IAW EO E1-53MR-260. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: MOUNT — CHAFED (RT ENGINE)
SAW - DURING INSPECTION, MAINTENANCE REPORTED THE RIGHT ENGINE OUTBOARD ZEE MOUNT CHAFED BY WIRE CONDUIT. MAINTENANCE REMOVED AND REPLACED THE ZEE MOUNT IAW JIC 54-21-61-RAI-10000-010. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: MOUNT — CORRODED (LEFT ENGINE)
SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE LEFT ENGINE OUTBOARD ZEE MOUNT MIDDLE TUBE PITTED. MAINTENANCE REMOVED AND REPLACED THE ZEE MOUNT IAW JIC 54-21-61-RAI-10000. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: PAN — CORRODED (CARGO BAY)
DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE CARGO DOOR UPPER AFT CORNER OF PAN CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAN IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: ANGLE — CORRODED (AFT CARGO BAY)
DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT AFT CARGO ZEE MEMBER CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: STRINGER — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED STRINGER 20R CORRODED BETWEEN FRAME 16 AND 17. MAINTENANCE REPAIRED STRINGER 20R IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: STRINGER — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED STRINGER 21L CORRODED BETWEEN FRAME 39 AND 40. MAINTENANCE REPAIRED STRINGER 21L IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: MOUNT — CHAFED (RT ENGINE)
SAW - DURING PHASE 2 INSPECTION, MAINTENANCE REPORTED THE RIGHT ENGINE W MOUNT CHAFED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE W MOUNT IAW JIC 54-11-61-RAI-10000-004. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SKIN — GOUGED (FUSELAGE)
SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED A GOUGE IN THE FUSELAGE BETWEEN FRAME 16 AND 17 NEAR STRINGER 17L. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-00-00 PAGE 410. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,265 hrs · 34,282 cycles
SAW - DURING PS-2 INSPECTION, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT 3WL IAW ATR AMM. OPS CHECKED GOOD. (X)
Part: BULKHEAD — CORRODED (FUSELAGE)
SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE AFT PRESSURE BULKHEAD HAD A SPOT OF CORROSION LOCATED AT 1:00 POSITION HALFWAY BETWEEN CENTER AND OUTER EDGE MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 53-00-00 PAGE 436. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAL — FAILED (RT ENGINE)
ORD - FLT 4236 - ABORTED TAKEOFF DUE TO RIGHT BLEED LEAK. ON TAXI BACK TO GATE RIGHT BLEED LEAK WITH BLEED OFF. WHILE PARKING FA TOLD FLT CREW SMOKE COMING OUT OF RIGHT ENGINE. EMERGENCY DECLARED. CFR RESPONDED PAX DEPLANED. NO EVIDENCE OF FIRE FOUND. FOUND RIGHT LEADING EDGE DUCT SEAL BAD. REMOVED AND REPLACED SEAL IAW ATR 42 JC 36-11-00. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,721 hrs · 33,453 cycles
SBN - FLT 4275 - FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING NEAR SEATS 2B, 3B, AND 5B INOPERATIVE. TOTAL OF THREE BULBS INOPERATIVE. C/A-REMOVED AND REPLACED FLOOR PROXIMITY AND EXIT SIGN POWER SUPPLY UNIT AND BATTERY PACK. OPS CHECK GOOD. REF: OPER CONTROL NR 20000815SH001. (X)
Part: POWER SUPPLY — UNKNOWN (CABIN) · airframe 24,721 hrs · 33,453 cycles
SBN - FLT 4275 - FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING NEAR SEATS 2B 3B, AND 5B INOPERATIVE. TOTAL OF THREE BULBS INOPERATIVE. C/A-REMOVED AND REPLACED FLOOR PROXIMITY AND EXIT SIGN POWER SUPPLY UNIT AND BATTERY PACK. OPS CHECK GOOD. REF: OPER CONTROL NR SIMA152-1. (X)
Part: BULB — FAILED (ROWS 2,3,&4) · airframe 24,633 hrs · 33,322 cycles
ORD - FLT 4262 - FLOOR PROXIMITY LIGHTS AT 2A AND 3/4A INOPERATIVE. INSTALLED NEW BULBS IN 2, 3, AND 4 A POSITIONS. OPS CHECKED GOOD. (X)
Part: LIGHT — INOPERATIVE (ROW 3)
ORD - FLT 4319 - FLOOR PROXIMITY LIGHT AT ROW 3 INOPERATIVE. REPAIRED CANNON PLUG AT 33WL. OPS CHECK GOOD. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 1AB TO 4AB. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 3WL IAW JIC 335121-RAI-10000. OPS CHECK GOOD. (M)
1999
Part: POWER SUPPLY — FAILED (CABIN)
CMI - FLT 4364 - CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE BY ROWS 2, 3 AND 5. REMOVED AND REPLACED POWER SUPPLY AT 29WL AND 10WL. OPS CHECK GOOD. (M)
Part: POWER SUPPLY — FAILED (CABIN)
CMI - FLT 4364 - CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE BY ROWS 2, 3 AND 5. REMOVED AND REPLACED POWER SUPPLY AT 29WL AND 10WL.OPS CHECK GOOD. (M)
Part: MOUNT — CHAFED (LT NACELLE)
SAW - DURING PS-2 INSPECTION, FOUND THE LEFT ENGINE BLEED AIR SHUTOFF VALVE HAD CHAFED THROUGH THE AFT OUTBOARD ZEE MOUNT. REMOVED AND REPLACED THE ZEE MOUNT IAW JIC 542161-RAI-1000-007. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 INSPECTION, SEVERAL CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION 18WL. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY PACK AT LOCATION 10WL WAS DISCHARGED. REMOVED AND REPLACED THE BATTERY PACK IAW JIC 33-51-20. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — DAMAGED (CABIN)
SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT OUTBOARD SEAT TRACK FLOORBEAM 35 DAMAGED. SPLICED FLOORBEAM IAW SRM 53-00-00 FIGURE 438. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: BULB — FAILED (CABIN)
ORD - FORWARD EMERGENCY EXIT SIGN DOES NOT FULLY ILLUMINATE. REMOVED AND REPLACED BULBS FOR EXIT LIGHT. OPERATIONAL CHECK GOOD. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
GRR - EMERGENCY FLOOR PROXIMITY LIGHTS AT SEAT MID-CABIN DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR MID-CABIN FLOOR PROXIMITY LIGHTS. OPERATIONAL CHECK GOOD. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
GRR - CABIN EMERGENCY FLOOR LIGHTING HAS LIGHTS INOP AND FWD CENTER ESCAPE SIGN INOP. RAI BATTERY PACK FOR POWER SUPPLY 10WL IAW ATR JIC, OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 CHECK, MAINTENANCE REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AT LOCATION 10WL AND 20WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 CHECK, MAINTENANCE REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AT LOCATION 10WL AND 20WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SKIN — DENTED (FUSELAGE)
SAW - DURING MBV-2 INSPECTION MAINTENANCE DISCOVERED A DENT IN THE FUSELAGE SKIN 24 INCH AFT OF PAX DOOR. MAINTENANCE REPAIRED THE DENT IAW SRM 51-21-27 FIGURE 403. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1997
Part: RELAY — BURNED (COCKPIT)
ORD - FLT 4311 - CREW SMELLED ELECTRICAL SMELL IN COCKPIT. MAINTENANCE FOUND A BURNED RELAY BASE AT RACK 91VU RELAY 14LG. RAI'D RELAY 14LG AND RELAY BASE 14LGA AS WELL AS CONTACT NR 2. PERFORMED OPS CHECK WITH NO ELECTRICAL ODOR NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FLT 3522 - EMERGENCY FLOOR LIGHTS IN VARIOUS POSITIONS WILL NOT COME ON OR GO OFF. REPLACED POWER SUPPLY AT 30WL AND 15WL PN 301-1180 SN 249 AND SN 229, AND 29WL PN 301-1151, SN 3689, SN 3944, AND SN 10488. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FLT 3635 - EMERGENCY LIGHTS CAME ON WHEN BATTERY SWITCH WAS TURNED OFF. RAI'D EMERGENCY BATTERY PACK AT 29WL, OPS CHECK GOOD. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DFW - FORWARD EMERGENCY LIGHT STRIP HAS THREE BULBS INOP. RAI'D POWER SUPPLY AND BATTERY PACKS 29WL. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (M)
Part: DC BPCU — FAILED (LEFT)
CID - FLT 4074 - NR 1 DC GENERATOR FAULTED, AIRCRAFT WAS DIVERTED TO CID AND LANDED SAFELY. AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR FERRY FLIGHT TO ORD, WHERE MAINTENANCE RAI'D DC BPCU, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ORD - FLT 4340 - EMERGENCY EXIT LIGHTING SYSTEM ILLUMINATES WITH ALL AIRCRAFT POWER, EXTERNAL POWER AND EMERGENCY LIGHT SYSTEM OFF. RAI'D EMERGENCY BATTERY PACK 15WL, OPS CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1996
Part: POWER SUPPLY — INOPERATIVE (CABIN)
ORD - FLT 4340 - EMERGENCY LIGHTS INOP AT ROW 1. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW ATR JOB CARD 33-51-21. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON THE RIGHT FORWARD OUTBOARD SEAT TRACK. MAINTENANCE REMOVED ADN REPLACED SEAT TRACK IAW EO 4-53-077. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SKIN — DENTED (FUSELAGE)
MQT - MAINTENANCE PERFORMING AN IMBV, FOUND A DENT RIGHT SIDE OF AIRCRAFT BETWEEN FRAME FRAME 41 AND 42. MAINTENANCE REPAIRED DENT WITH SKIN PATCH IAW EO E1-5300-178. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOOR BEAM — CORRODED (FUSELAGE)
MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON FLOOR BEAM 36. MAINTENANCE REMOVED REPLACED FLOOR BEAM IAW EO E9-5300-004. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: GUSSET — CRACKED (RT MLG WW)
MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND A CRACK IN THE RIGHT WHEEL WELL GUSSET AT FRAME 25, STRINGER 14. MAINTENANCE REPAIRED GUSSET WITH A STAINSTEEL DOUBLER IAW EO E1-5300-190. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION AROUND 5 HI-LOKS ON A DOUBLER LOCATED AT FRAME 25 BETWEEN STRINGER 14 AND 15 ON RIGHT SIDE OF AIRCRAFT. MAINTENANCE REMOVED CORROSION BY SPOT FACING BLENDING AND APPLYING ALODINE IAW EO E1-5300-195. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON THE LEFT FORWARD OUTBOARD SEAT TRACK. MAINTENANCE REMOVED AND REPLACED SEAT TRACK IAW EO 4-53-077. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON LEFT AFT SEAT TRACK OF FRAME 39. MAINTENANCE REMOVED AND REPLACED SEAT TRACK IAW EO E95300-002. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: WINDOW FRAME — CORRODED (FUSELAGE)
MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION BEYOND LIMITS ON THE WINDOWS FRAME RIGHT SIDE NR 3 THRU 18, AND LEFT SIDE NR 2 THRU 12, AND 14 THRU 17. MAINTENANCE REMOVED AND REPLACED ABOVE NUMBERED WINDOWS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)
1995
Part: ATTACH BOLT — LOOSE (WING FITTING)
FUEL SEEPAGE FOUND AT LEFT REAR WING ATTACHMENT BOLT AT RIB NR 4 LOCATED AT LEFT AFT INSTALLATION FITTING. FOUND LEFT WING ATTACHMENT AFT FITTING BOLT LOOSE. NEW BOLT WAS INSTALLED AND AREA INSIDE THE FUEL TANK WAS SEALED AS PER STRUCTURAL REPAIR MANUAL CHAPTER 517120.