N19504
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.
19 reports on file, 1995-02-09 – 1998-02-19.
Part: LATCH MECHANISM — INOPERATIVE (LT MLG DOOR)
UPLATCH CHECK WAS UNSATISFACTORY. THE LEFT GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS WERE ILLUMINATED. THE GEAR WAS RECYCLED AND RECHECKED, BUT WAS STILL UNSATISFACTORY. OPERATION WAS CONTINUED AT BELOW .70 MACH WITH RIGHT ENGINE HYDRAULICS ON HIGH. MAINTENANCE FOUND THE LT MLG DOOR LATCH MECHANISM AT FAULT, ALLOWING THE DOOR TO DROOP WITH HYDRAULIC POWER OFF. THE LATCH MECHANISM WAS REMOVED AND REPLACED IAW MM 32-31-4, PAGES 201-210.
Part: SENSOR — INOPERATIVE (RT DE-ICE SYST)
THE RT AIR CONDITIONING SUPPLY TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF WITH SMOKE IN THE CABIN. THE AIRFOIL ICE PROTECTION WAS ON. THE PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE RT ICE PROTECTION HIGH TEMP SENSOR WAS REMOVED AND REPLACED IAW MM 30-10-6. THE ENGINES WERE RUN WITH PACKS OPERATING AND NO DEFECTS WERE NOTED.
Part: BEAM — CRACKED (CABIN DOOR)
INSPECTION FOUND, A 1.25 INCH CRACK IN NR 1 BEAM, A .75 INCH CRACK IN NR 2 BEAM, AND A .5 INCH CRACK IN NR 3 BEAM OF MAIN CABIN DOOR. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-05, FIGURE 31.
Part: PAN — CRACKED (CABIN DOOR)
INSPECTION FOUND, A 6 INCH CRACK AT AFT UPPER CORNER OF MAIN CABIN DOOR PAN. THE AREA WAS REPAIRED IAW ECRA 5211-01020.
Part: FITTING — CRACKED (RT WING/FUS)
INSPECTION FOUND A 3 INCH CRACK IN RT WING TO FUSELAGE ATTACH FITTING AT FRONT SPAR. A STRAP WAS INSTALLED ON WING TO FUSELAGE ATTACH ANGLE IAW ECRA 5340-0100.
Part: SUPPORT — CORRODED (BS 160-200)
INSPECTION FOUND FLOOR SUPPORT FORWARD OF LEFT OUTBOARD SEAT TRACK CORRODED AT STA 160-200. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.
Earlier reports · 1995–1997 · 13 reports
1997
Part: SOCKET — DIRTY (NLG)
THE NLG DID NOT INDICATE GREEN SAFE WHEN GEAR WAS EXTENDED FOR LANDING. AN EMERGENCY LANDING WAS DECLARED AND ALTERNATE GEAR EXTENSION WAS USED. BOTH THE LT AND RT INBOARD MLG DOORS WERE DAMAGED ON LANDING. THE LEFT INBOARD MLG DOOR WAS REMOVED AND REPLACED IAW MM 32-12-1. THE RT INBOARD MLG DOOR WAS REPAIRED IAW ECRA 5280-01164, FERRIED FOR PERMANENT REPAIR. COULD NOT DUPLICATE THE FAULT. THE NLG DOWNLOCK SWITCH WAS INSPECTED WITH NO TROUBLE FOUND. THE NLG GREEN LIGHT SOCKET ASSEMBLY WAS CHECKED AND CLEANED, OPERATIONAL CHECKS AND INDICATIONS WERE GOOD.
1996
Part: CONTROLLER — INOPERATIVE (LT PACK)
SHORTLY AFTER TAKEOFF, THE LT PACK VALVE WENT TO FULL HOT IN AUTO, THE CONTROL WAS SWITCHED TO MANUAL AND MODULATED TO COLD. THE PACK VALVE DID NOT RESPOND AND THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE PACK AUTO SHUTDOWN, BUT THE SMOKE CONTINUED. THE AIRCRAFT WAS RETURNED TO MDW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT PACK TEMP CONTROLLER AT FAULT. THE TEMP CONTROLLER WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE NOTED.
Part: BULBS — FAILED (LANDING GEAR)
THE RT MLG DID NOT INDICATE DOWN AND LOCKED WITH GEAR HANDLE DOWN NOR WITH ALTERNATE EXTENSION WHILE ON APPROACH. THE GEAR WAS CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LANDING GEAR ANNUNCIATOR LAMPS BURNED OUT. THE LANDING GEAR ANNUNCIATOR LAMPS WERE REPLACED AND ALL INDICATIONS WERE NORMAL.
Part: DRIVE LINK — BROKEN (LT ENG TR)
MTY - FLT 0705 - THE LEFT ENGINE REVERSE UNLOCK LIGHT ILLUMINATED ON LANDING AT MTY. MAINTENANCE FOUND A LEFT ENGINE THRUST REVERSER DRIVE LINK BROKEN. THE DRIVE LINK REMOVED AND REPLACED. OPERATION CHECKED GOOD PER MM 78-31-5, PAGES 201-207, FIGURE 201. (X)
Part: CONNECTOR — FAILED (RT COFFEE MAKER)
IAH - FLT 1809 - WHITE SMOKE WITH BURNING ELECTRICAL SMELL ENTERED THE COCKPIT ON APPROACH TO IAH. THE SMOKE AND SMELL DISSIPATED AFTER TURNING OFF THE GALLEY POWER AND PULLING ALL CIRCUIT BREAKERS IN GALLEY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CANNON PLUG ON RT COFFEEMAKER BURNED. THE CONNECTOR PLUG WAS REPLACED. OPERATION OF BOTH THE RT AND LT COFFEEMAKERS CHECKED GOOD. (X)
Part: LANYARD — FRAYED (SERVICE DOOR)
HOU - INSPECTION FOUND THE FORWARD SERVICE DOOR SLIDE LANYARD CABLE FRAYED. THE LANYARD WAS REMOVED AND REPLACED. (M)
Part: SPAR CAP — CRACKED (RT TE FLAP)
HOU - INSPECTION FUOND A 1.5 INCH CRACK IN RIGHT FLAP SPAR CAP AT INBOARD ATTACH FITTING, OUTBOARD FIXED VANE. THE CRACKED AREA WAS CUT OUT. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5710-01719 AND SRM 57-01. (M)
Part: INTERCOSTAL — CRACKED (MAIN CABIN DOOR)
HOU - INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REPAIRED IAW SRM 52-05, FIGURE 45. (M)
Part: BEAM — CRACKED (MAIN CABIN DOOR)
HOU - INSPECTION FOUND A .5 INCH CRACK NR 5 BEAM OF MAIN CABIN DOOR. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31, SHEET 6. (M)
Part: BEAM — CRACKED (MAIN CABIN DOOR)
INSPECTION FOUND A .5 INCH CRACK IN NR 8 BEAM OF MAIN CABIN DOOR. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 31, SHEET 9. (M)
Part: BLKHD T-CAP — CORRODED (BS 110)
HOU - INSPECTION FOUND T-CAP CORRODED AT AFT BULKHEAD STATION 110 IN NLG WHEEL WELL RIGHT TUNNEL. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED IAW SRM 51-10-3. (M)
1995
Part: CSD WASHER — BROKEN (NR 1 ENG)
FLT 1804 - CLE - THE NR 1 ENGINE EXPERIENCED AN UNCOMMANED SHUT DOWN ON FINAL APPROACH TO CLE. THE LANDING WAS UNEVENTFUL. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK CHECK AND POWER ASSURANCE RUN WERE GOOD. SHOP FINDINGS REVEALED CSD REAR BEARING SHAFT LOCKING WASHER HAD BROKEN TANGS. (M)
Part: RADAR IND — INOPERATIVE (COCKPIT)
OKC - FLT 1468 - THE RADAR WENT INOPERATIVE AND WAS ACCOMPANIED BY A BURNING ODOR WHILE EN ROUTE TO OKC. THE RADAR WAS TURNED OFF AND THE ODOR SUBSIDED. THE FLIGHT WAS CONTINUED AND THE ACFT LANDED AT OKC WITHOUT INCIDENT. MAINTENANCE FOUND THE RADAR INDICATOR AT FAULT. THE RADAR INDICATOR WAS REPLACED AND RADAR OPERATION CHECKED GOOD. (W)