N927VJ
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
32 reports on file, 1995-02-03 – 2000-11-21.
Part: CHARGER — FAILED (CABIN)
PIT - THE AFT SECTION OF THE FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR EMERGENCY LIGHTS CHARGER. (M)
Part: CHARGER — FAILED (CABIN)
IND - THE AFT SECTINO OF THE FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
Part: POWER SUPPLY — FAILED (CABIN)
PHL - SEVERAL FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR TRACK EMERGENCY LIGHT BATTERY AND POWER SUPPLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 9 THROUGH 12 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
Part: POWER SUPPLY — FAILED (PAX CABIN)
IND - THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 9 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
DAY - THE AFT FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY LIGHT BATTERIES. (M)
Part: MANIFOLD — LEAKING (RT ENGINE)
CLT-DAY FLT 860 - AFTER TAKEOFF, THE RIGHT ENGINE FIRE INDICATION ACTIVATED. THE THROTTLE WAS REDUCED AND THE INDICATION STOPPED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE THE RIGHT ENGINE FUEL HEAT MANIFOLD. (M)
Part: KEEL BEAM — CHAFED (BS 917)
PIT - STA 917 A/C CENTERLINE. BEAM CAP HAD 1 INCH BY 2 INCH CHAFE MARK. KEEL BEEM FOUND CRACKED AT BS 917. BLENDED OUT WEAR MARKS AND INSTALLED .025 INCH SS WEAR STRIP PER SRM 53-05 FIG 20 PAGE 30A. (X)
Part: ANGLE — CRACKED (VERTICAL STAB)
PIT - REMOVED AND REPLACED VERTICAL STABILIZER DRAG ANGLE, STA 1104. DRAG ANGLE HAD 2 INCH CRACK. DRAG ANGLE FOUND CRACKED ON VERTICAL STABILIZER. STOP DRILLED CRACK ENDS AND INSTALLED REPAIR PER SRM 53-05 FIG 23 AND 23A. (X)
Part: BULKHEAD — CRACKED (BS 965)
PIT - RIGHT SIDE STA 965 BULKHEAD WEB LOWER END, WEB HAD 2 INCH CRACK. BULKHEAD FOUND CRACKED AT BS 965. CUT OUT DAMAGED WEB SECTION AND INSTALLED NEW PER SRM 53-03 FIG 19. (X)
Part: FRAME — CRACKED (BS 109.5)
PIT - STA 109.5 CANTED BELTRAME. WEB HAD 3.50 INCH CRACK. BELT FRAME FOUND CRACKED AT BS 109.5. REPAIRED PER EA 53797. (X)
Part: ANGLE — CRACKED (VERTICAL STAB)
PIT - LEFT VERTICAL STABILIZER DRAG ANGLE, STA 1104. DRAG ANGLE HAD 2 CRACKS, .75 INCH AND .3750 INCH. DRAG ANGLE FOUND CRACKED ON VERTICAL STABILIZER. CUT OUT DAMAGED AREA AND INSTALLED STRAP PER SRM 53-05 FIG 23A (DASH 505 CONFIG). (X)
Part: SKIN — CRACKED (BS 180)
PIT - LONGERON 22L BELOW AIR STAIR, SKIN HAD .25 INCH CRACK. SKIN CRACKED AT BS 180 LONGERON 22L. PERMANENT REPAIR DOUBLER INSTALLED PER SRM 9530219 AND EO 53910467. (X)
Part: BEAM — CORRODED (FUSELAGE)
PIT - FOUND BEAM CORRODED IN 2 AREAS, 1 INCH BY 1 INCH. CORROSION LEVEL 1. CUT OUT CORRODED AREAS AND INSTALLED NESTED ANGLE. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PIT - STATION 160 A/C CENTERLINE RIGHT FLOOR SUPPORT HAS 2 INCH BY 36 INCH CORROSION. LEVEL 1. MANUFACTURE NEW SUPPORT AND INSTALLED. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
PIT - LEFT INBOARD SEAT TRACK STATION 237 HAS CORROSION 2 INCH BY 4 INCH. CORROSION LEVEL 1. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)
Earlier reports · 1995–1999 · 16 reports
1999
Part: CHARGER — FAILED (CABIN)
IND - THE AFT CABIN AND TAIL COMPARTMENT FLOOR TRACK EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN AND TAIL COMPARTMENT FLOOR TRACK EMERGENCY LIGHT BATTERY CHARGER. (M)
Part: SUPPLY — FAILED (CABIN)
THE ENTRANCE AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE ENTRANCE AREA EMERGENCY LIGHTS POWER SUPPLY AND BATTERIES. (M)
Part: UNION — LOOSE (LT ENGINE)
PHL-ATL - FLT 1243 - DURING CLIMB-OUT, THE LEFT ENGINE REQUIRED HIGHER THROTTLE SETTINGS TO MAINTAIN EQUAL EPR READINGS. THE HIGHER THE ALTITUDE THE GREATER THE THROTTLE SPREAD BETWEEN THE TWO ENGINES. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE UNION AT THE PT2 FLEX HOSE. (M)
Part: WIRE — CHAFED (CABIN)
PHL - THE LAST FOUR SEAT ROWS AND THE ENTIRE TAIL SECTION EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED A CHAFFED WIRE AT SEAT ASSEMBLY 21 E/F. (M)
Part: ENGINE — FAILED (LEFT)
PHL-SYR - FLT 725 - AFTER TAKEOFF, THE LEFT ENGINE DEVELOPED COMPRESSOR STALLS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. (M)
Part: FRAME — CRACKED (BS 1095)
PIT - PHL MAINTENANCE FOUND 3.5 INCH CRACK AT BELT FRAME WEB STATION 1095 LEFT SIDE. INSTALLED TEMPORARY DOUBLER PER EA 52499. (M)
1998
Part: LONGERON — CRACKED (BS 639)
PIT - DURING C-6 CHECK, FOUND LONGEORN CRACKED ACROSS INTERSECTION .20 INCH AT STATION 639 LONGERON 4L. INSTALLED SPLICE PER SRM 53-02 PAGES 48-53. (M)
Part: POWER SUPPLY — FAILED (CABIN)
CMH - THE CEILING EMERGENCY EVACUATION LIGHTS FOR THE CENTER SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERENCY LIGHT POWER SUPPLY. (X)
Part: VALVE — LEAKING (NLG STRUT)
LGA - FL 475 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RAISE AND THERE WAS AN UNSAFE NOSE GEAR INDICATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND REPLACED THE SCHRADER VALVE. (X)
1997
Part: BATTERY PACK — DISCHARGED (CABIN)
CMH - AFT FLOOR TRACK EMERGENCY LIGHTING IS PARTIALLY INOPERATIVE AND PARTIALLY DIM. MAINTENANCE REPAIRED THE EMEREGENCY FLOOR TRACK WIRING AND REPLACED THE POWER SUPPLY AND BATTERY PACK. (M)
Part: POWER SUPPLY — FAILED (CABIN)
CMH - AFT FLOOR TRACK EMERGENCY LIGHTING IS PARTIALLY INOPERATIVE AND PARTIALLY DIM. MAINTENANCE REPAIRED THE EMEREGENCY FLOOR TRACK WIRING AND REPLACED THE POWER SUPPLY AND BATTERY PACK. (M)
Part: POWER SUPPLY — FAILED (TAILCONE)
CMH - FOUND TAILCONE AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. (M)
1996
Part: POWER SUPPLY — FAILED (RT NACELLE)
RIGHT SIDE NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REPLACED POWER PACK. (M)
Part: RMI — FAILED (RT COCKPIT)
PIT - FL 1036 - UPON REACHING FL 180 OUT OF PIT, CREW NOTED BOTH RIM'S SPINNING AND COULD NOT FIX THE AIRCRAFT POSITION. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT RMI. (M)
Part: SLIDE — FAILED (FWD GALLEY DR)
FLT NR 517 - PHL - GALLEY EMERGENCY CHUTE PRESSURE IS 2500 PSI IN RED ZONE. REPLACED GALLEY EMERGENCY CHUTE. (M)
1995
Part: UPLATCH ROLLER — LOOSE (RT MLG)
CAE - FLT 0253 - ON LANDING IN CAE, THE GEAR DOOR OPEN LIGHT WOULD NOT GO OUT. THE GEAR WAS RECYCLED THREE TIMES BUT THE LIGHT REMAINED ON. MAINTENANCE SECURED A LOOSE ROLLER ON THE RIGHT MAIN LANDING GEAR UPLATCH. CHECKED OTHER PORTIONS OF THE DOOR INDICATION SYSTEM. NO DEFECTS WERE NOTED. GEAR WAS SWUNG SEVERAL TIMES. ALL INDICATIONS WERE NORMAL. (W)