N24213
Registered owner: CAREER TRACK 1 LLC, DE (owner ≠ operator)
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.
20 reports on file, 1995-09-11 – 1997-05-15.
Part: BATT CHARGER — BURNED (E\E COMPT)
AN ELECTRICAL ODOR WITH A SLIGHT TRACE OF HAZE WAS NOTICED IN THE CABIN WHILE ON DESCENT INTO CLE. THE GASPER FAN AND GALLEY POWER WAS TURNED OFF AND THE ODOR DECREASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BATTERY CHARGER IN E AND E COMPARTMENT BURNED. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND TESTED IAW MM 24-31-21. OPERATIONAL CHECKS WERE GOOD WITH NO EVIDENCE OF ODOR OR SMOKE.
Part: STRUT — CRACKED (LT MLG)
A GRINDING SOUND WAS HEARD COMING FROM LANDING GEAR AREA DURING TAXI. MAINTENANCE FOUND THE NR 2 BRAKE ASSEMBLY DAMAGED DUE TO A SHEARED BOLT AND THE LT MLG INNER CYLINDER WAS CRACKED. THE LT MLG INNER CYLINDER WAS REMOVED AND REPLACED. IN ADDITION, THE NR 2 BRAKE, TIRE ASSEMBLY WERE REMOVED AND REPLACED.
Part: FAN — INOPERATIVE (CABIN)
THE FLIGHT ATTENDANTS REPORTED, A BURNING ODOR IN CABIN WHILE EN ROUTE. THE SMOKE CHECKLIST PROCEDURE WAS ACCOMPLISHED AND THE ODOR DISSIPATED AFTER THE RT PACK WAS SHUTDOWN. THE AIRCRAFT LANDED AT PVD WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE AIR DISTRIBUTION FAN WAS FOUND INOPERATIVE WITH THE CIRCUIT BREAKER POPPED. THE AIR DISTRIBUTION FAN WAS PLACARDED INOPERATIVE. IN ADDITION, THE RT PACK WAS PLACARDED INOPERATIVE AS A PRECAUTIONARY MEASURE.
Earlier reports · 1995–1996 · 17 reports
1996
Part: RELAY MODULE — BURNT (COCKPIT)
SMOKE WITH FUMES WAS OBSERVED COMING FROM ELECTRICAL PANEL BY THE JUMP SEAT ON AIRCRAFT RIGHT ON APPROACH. THE M181 MODULE WAS HOT TO TOUCH, THE MODULE WAS REMOVED AND SMELLED BURNT. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE M181 RELAY MODULE. THE MODULE TESTED GOOD AND NO OTHER DISCREPANCIES WERE FOUND.
Part: DRIVE MECHANISM — WORN BEARING (LT TE FLAP)
WHEN FLAPS WERE SELECTED TO 30 DEGREES ON APPROACH, THE AIRCRAFT ROLLED LEFT. THE FLAPS WERE SET TO 25 DEGREES AND THE ROLL STOPPED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT INBOARD AFT FLAP STICKING IN THE UP POSITION WITH FLAPS LOWERED. THE LEFT INBOARD AFT FLAP DRIVE MECHANISM HAD A WORN CENTER BEARING. THE FLAP DRIVE MECHANISM WAS REPLACED. THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO DEFECTS. IN ADDITION, THE LEFT INBOARD TRAILING EDGE FLAP WAS ADJUSTED/TESTED IAW MM 27-51-12, PAGES 501 TO 506.
Part: ANGLE — CORRODED (NLG WW)
INSPECTION FOUND NOSE WHEEL WELL CEILING SUPPORT I BEAM AND ATTACHING ANGLES CORRODED. THE BEAM AND ANGLES WERE REMOVED. A NEW BEAM AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-5, 51-30-2 AND 51-10-2.
Part: FRAME — CRACKED (C-1 DOORWAY)
INSPECTION FOUND A 3 INCH CRACK IN UPPER FLANGE OF C-1 DOORWAY AFT FRAME. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BOEING DRAWING 65C35242.
Part: SKIN — DENTED (BS 1016)
INSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 1016, S29R. THE DENTED AREAS WERE CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 SRM 51-30-2 AND 51-10-2.
Part: STRINGER — CORRODED (BS 351.5-360)
INSPECTION FOUND STRINGER CHANNEL CORRODED AT STA 351.2 TO 360, S20L. THE STRINGER CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND BOEING DRAWING 69-48934.
Part: SKIN — DENTED (BS 394)
INSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6.
Part: SKIN — DENTED (BS 394)
INSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6.
Part: SKIN — CREASED (BS 228-360)
INSPECTION FOUND SKIN CREASED FROM BS 228 TO 360, JUST ABOVE STRINGER 19R. THE DAMAGED SKIN WAS CUT OUT, REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 16.
Part: STRINGER — CORRODED (BS 416)
INSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.
Part: SKIN — CORRODED (BS 410)
INSPECTION FOUND SKIN CORRODED AT BS 410, STRINGER 18L. THE CORRODED SKIN WAS CUTOUT. A REPAIR DOUBLER AND FILLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6.
Part: FLOORBEAM — CORRODED (BS 294.5)
INSPECTION FOUND CORROSION ON AFT UPPER FLANGE OF FLOORBEAM AT BS 294.5, RBL 20 TO RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW SECTION OF FLOORBEAM AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 FIGURE 1.
Part: STRINGER — CORRODED (BS 390-410)
INSPECTION FOUND CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRINGER WAS REMOVED. REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.
Part: SKIN — DENTED (BS 344-380)
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 TO 380, STRINGER 20R TO 22R. THE DENTED AREA OF SKIN WAS CUT OUT AND NEW SKIN, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 AND 9, SRM 51-10-2 AND 51-30-2.
1995
Part: ANGLE — CRACKED (BS 664)
GSO - INSPECTION FOUND A 2.5 INCH CRACK IN RADIUS OF RT LOWER FORWARD SHEAR BEAM ATTACH ANGLE AT STA 664. THE CRACKED ANGLE WAS REMOVED AND SHEAR BEAM MODIFICATION KIT PART NR 5310-02450-10 WAS INSTALLED IAW EA 5310-02450. (X)
Part: FLOOR BEAM — CRACKED (BS 700-717)
GSO - INSPECTION FOUND FLOOR BEAM WEB CRACKED AT FIVE EACH LOWER FASTENER HOLES BETWEEN BS 700-BS 717, BBL 0.07. THE COMBINED CRACK LENGTH WAS APPROXIMATELY 5 INCHES. THE CRACKED SECTION OF WEB WAS REMOVED AND A NEW WEB AND DOUBLER WERE FABRICATED AND INSTALLED IAW EA 5710-01322. (X)
Part: SKIN — CORRODED (BS 400)
IAH - INSPECTION FOUND A POPPED FASTENER WITH CORROSION IN SKIN AT LAP JOINT FORWARD OF C-1 DOOR THRESHOLD STATION 400. THE CORRODED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 16. (M)