# N14524: Mcdonnell Douglas DC-9-32, registration cancelled 2000-05-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 31, 2000 - Exported to: Venezuela - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47539 - Type of aircraft: Fixed wing multi engine - Certificate issued: December 3, 1999 - Last registry action: December 3, 1999 - Mode S code: A0B7FE - Owner when cancelled: [Aeroturbine Inc](https://openairdocs.org/faa-owner/AEROTURBINE%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14524 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14524 - Page: https://openairdocs.org/deregistered/N14524-2000-05-31 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md ## Service difficulty reports (50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9900209](https://openairdocs.org/sdr/CALA9900209), Mar 2, 1999: WIRE. BROKEN. INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND LIGHT WIRE PULLED FROM SPLICE. THE WIRE WAS RESPLICED AND OPERATION CHECK - [SDR CALA9900208](https://openairdocs.org/sdr/CALA9900208), Mar 2, 1999: BATTERIES. DISCHARGED. INSPECTION FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9900207](https://openairdocs.org/sdr/CALA9900207), Mar 1, 1999: BATTERIES. DISCHARGED. INSPECTION FOUND THE TAIL CONE EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9900105](https://openairdocs.org/sdr/CALA9900105), Feb 2, 1999: WIRE. LOOSE. THE AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH WAS FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE ON SWITCH. THE LOOSE WIRE WAS TIGHTENED AND SYSTEM - [SDR CALA9900104](https://openairdocs.org/sdr/CALA9900104), Feb 2, 1999: WIRE. BROKEN. THE AFT CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 23 TO TAIL SECTION. MAINTENANCE FOUND WIRING TO BATTERY POWER PACKS BROKEN. THE WIRING WAS REPA - [SDR CALA9900103](https://openairdocs.org/sdr/CALA9900103), Feb 2, 1999: WIRE. BROKEN. THE CABIN EMERGENCY LIGHTS FROM COCKPIT TO ROW 13 WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PA - [SDR CALA9900102](https://openairdocs.org/sdr/CALA9900102), Feb 2, 1999: WIRE. BROKEN. THE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0 - [SDR CALA9900096](https://openairdocs.org/sdr/CALA9900096), Jan 30, 1999: CONNECTOR. DIRTY. INSPECTION FOUND THE L-1 PORTABLE EMERGENCY LIGHT INOPERATIVE. THE CONNECTOR WAS CLEANED AND SECURED AND OPERATION OF THE LIGHT CHECKED GOOD. - [SDR CALA9900093](https://openairdocs.org/sdr/CALA9900093), Jan 29, 1999: WIRE. BROKEN. INSPECTION FOUND THE ESCAPE PATH LIGHT INBOARD OF FORWARD FIRST CLASS COAT CLOSET INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING. THE ESCAPE PATH LIGHT WIRING WAS - [SDR CALA9900092](https://openairdocs.org/sdr/CALA9900092), Jan 28, 1999: FITTING. CRACKED. INSPECTION FOUND AFT CARGO DOOR THIRD BEAM END FITTING CRACKED AT AFT SIDE OF DOOR. THE CRACK WAS .1875 INCH LONG. THE FITTING WAS REMOVED AND A NEW FITTING WAS - [SDR CALA9900084](https://openairdocs.org/sdr/CALA9900084), Jan 27, 1999: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR BEAM END FITTING AT AFT SIDE OF DOOR. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5 - [SDR CALA9900037](https://openairdocs.org/sdr/CALA9900037), Jan 20, 1999: RIB. CRACKED. RIB CRACKED THROUGH FASTENER HOLE INSIDE LEFT WING L/E XRS545 (.5) 12 INCES OUTSIDE OF NR 5 SLAT CENTER TRACK. REMOVED AND INSTALLED NEW RIB PER SRM 51-30-2. - [SDR CALA9900062](https://openairdocs.org/sdr/CALA9900062), Jan 16, 1999: TAB. DEBOND. RIGHT AILERON INBOARD TAB HAS APPROXIMATELY 1 BY 10 DEBONDED LOWER SKIN. REMOVED AND REPLACED RIGHT AILERON PER MM 27-10-2. - [SDR CALA9900011](https://openairdocs.org/sdr/CALA9900011), Jan 13, 1999: ANGLE. CRACKED. RIB TO LOWER LE ANGLE CRACKED INSIDE RIGHT WING APPROX 8 O/B OF VORTILON. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-5, 51-10-0, 51 - [SDR CALA9900010](https://openairdocs.org/sdr/CALA9900010), Jan 11, 1999: TERMINAL. FAILED. AFT DOOR EMERGENGY EXIT LIGHT INOP. REPAIRED TERMINAL AT LIGHT AND OPS CHECK OK PER MM 33-53-01. - [SDR CALA9900101](https://openairdocs.org/sdr/CALA9900101), Jan 2, 1999: SPAR. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN RT WING AFT SPAR AT I/B ACTUATOR HINGE FORWARD FORGING FROM I/B LOWER BOLT AREA, APPROXIMATELY XRS 164. THE FASTENERS WERE - [SDR CALA9900004](https://openairdocs.org/sdr/CALA9900004), Jan 3, 1998: CONTROL. INOP. THE LT MLG UNSAFE LIGHT ILLUMINATED ON UPLATCH CHECK AFTER TAKEOFF. WHEN THE SLATS AND FLAPS WERE EXTENDED TO FIVE DEGREES AND THE AIRCRAFT WAS SLOWED TO 210 KN - [SDR CALA9701678](https://openairdocs.org/sdr/CALA9701678), Nov 24, 1997: SPAR CAP. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE - [SDR CALA9701660](https://openairdocs.org/sdr/CALA9701660), Nov 20, 1997: SPAR CAP. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF LT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE - [SDR CALA9701659](https://openairdocs.org/sdr/CALA9701659), Nov 20, 1997: SPAR CAP. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER UPPER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE - [SDR CALA9701658](https://openairdocs.org/sdr/CALA9701658), Nov 20, 1997: SKIN. DENTED. INSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 323, LONGERON 24. THE DENTED AREA WAS CUT OUT IAW SRM 53-04. A DOUBLER, FINGER DOUBLER, AND FILLER WERE FABRICATE - [SDR CALA9701657](https://openairdocs.org/sdr/CALA9701657), Nov 20, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION ON FLOORBEAM NUT PLATE AT STA 965. A DOUBLER, FILLER, AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-30-5, AND ECRA 532 - [SDR CALA9701656](https://openairdocs.org/sdr/CALA9701656), Nov 20, 1997: FLOOR PANEL. CORRODED. INSPECTION FOUND FLOOR PANEL AND HAT CHANNEL CORRODED UNDER PILOT'S SEAT. A NEW PANEL AND HAT CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-20-0. - [SDR CALA9701655](https://openairdocs.org/sdr/CALA9701655), Nov 20, 1997: JAMB. CORRODED. INSPECTION FOUND DOOR JAMB AND SUB FLOOR CORRODED AT FS 200 BY R-1 DOOR. THE CORRODED DOOR JAMB PAN AND SUB FLOOR SECTIONS WERE REMOVED IAW SRM 53-05, FIGURE 55 - [SDR CALA9701654](https://openairdocs.org/sdr/CALA9701654), Nov 20, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT AT FORWARD PASSENGER ENTRYWAY CORRODED BETWEEN NR 1 SEAT TRACK AND CENTERLINE FLOORBEAM. THE FLOOR SUPPORT WAS REMOVED, A NE - [SDR CALA9701653](https://openairdocs.org/sdr/CALA9701653), Nov 20, 1997: SKIN. DENTED. INSPECTION FOUND DENTS IN E AND E COMPARTMENT DOOR EXTERIOR SKIN. THE SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-3. - [SDR CALA9701581](https://openairdocs.org/sdr/CALA9701581), Nov 3, 1997: LONGERON. CORRODED. INSPECTION FOUND LONGERON 25R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 218. THE LONGERON WAS REMOVED IAW SRM 53-10-03. A NEW LONGERON AND SPLICE SECTION WER - [SDR CALA9701580](https://openairdocs.org/sdr/CALA9701580), Nov 3, 1997: DOUBLER. GOUGED. INSPECTION FOUND GOUGED DOUBLER AT FORWARD PASSENGER DOOR CUTOUT FOR DOOR LATCH HOOK ASSEMBLY. THE OLD DOUBLER WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS FABRIC - [SDR CALA9701579](https://openairdocs.org/sdr/CALA9701579), Nov 3, 1997: LONGERON. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1079. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02. A REPAIR SECTION, SPLICE AND ATTACH BRACK - [SDR CALA9701578](https://openairdocs.org/sdr/CALA9701578), Nov 3, 1997: COVER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT ELEVATOR FLIGHT TAB MECHANISM CONTROL COVER AT STA XHS 95. THE CRACKED AREA WAS REMOVED, DOUBLER AND FILLER WERE FABRICATE - [SDR CALA9701577](https://openairdocs.org/sdr/CALA9701577), Nov 3, 1997: SKIN. DENTED. INSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 360 BETWEEN LONGERON 21R AND 22R. THE DENTED AREA WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INS - [SDR CALA9701519](https://openairdocs.org/sdr/CALA9701519), Oct 30, 1997: INTERCOSTAL. DENTED. INSPECTION FOUND INTERCOSTAL DENTED BETWEEN STA 560 AND 579 AT LONGERON 28R. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9701518](https://openairdocs.org/sdr/CALA9701518), Oct 30, 1997: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT STA 680-699, LONGERON 16L. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED - [SDR CALA9701517](https://openairdocs.org/sdr/CALA9701517), Oct 30, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND INTERCOSTAL CRACKED INSIDE R-1 DOOR AT CENTER OF DOOR BELOW LATCH MECHANISM. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30 - [SDR CALA9701516](https://openairdocs.org/sdr/CALA9701516), Oct 29, 1997: SKIN. DENTED. INSPECTION FOUND RT WING NR 1 LEADING EDGE SLAT SKIN DENTED. THE DENTED AREA WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 57-0 - [SDR CALA9701515](https://openairdocs.org/sdr/CALA9701515), Oct 29, 1997: STIFFENER. CRACKED. INSPECTION FOUND A 2 CRACK IN HORIZONTAL STIFFENER ON FORWARD FACE OF AFT PRESSURE BULKHEAD AT L13R. THE STIFFENER WAS REMOVED. NEW PARTS WERE FABRICATED AND IN - [SDR CALA9701514](https://openairdocs.org/sdr/CALA9701514), Oct 29, 1997: SKIN. DENTED. INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 284, LONGERON 24. THE DENTED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-04 AND 53-04, F - [SDR CALA9700111](https://openairdocs.org/sdr/CALA9700111), Jan 29, 1997: HYD LINE. LEAKING. THE RT HYDRAULIC SYSTEM LOST ALL QUANTITY DURING FLIGHT. ABNORMAL PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUN - [SDR CALA9601541](https://openairdocs.org/sdr/CALA9601541), Oct 31, 1996: DUCT. CRACKED. THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED SHORTLY AFTER TAKEOFF. THE FIRE WARNING CEASED AFTER THE ENGINE THROTTLE WAS RETARDED LESS THAN TEN PERCEN - [SDR CALA9600769](https://openairdocs.org/sdr/CALA9600769), Jun 7, 1996: PUSHROD. BENT. THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND PUSHROD AT GROUND SENSE SECTOR BENT. THE PUSHROD - [SDR CAL951140](https://openairdocs.org/sdr/CAL951140), Dec 7, 1995: FLOOR WEB. CRACKED. IAH - INSPECTION FOUND A 1 INCH CRACK IN COCKPIT FLOOR WEB AT BS 89.050 AND A 2 INCH CRACK FOUND AT BS 83.550. THE FLOOR WEB WAS REPAIRED IAW ECRA 5310-03193 AN - [SDR CAL950804](https://openairdocs.org/sdr/CAL950804), Aug 27, 1995: LONGERON. CORRODED. HOU - INSPECTION FOUND CORROSION ON LONGERON 26L BETWEEN STATION 945-960. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE INSTALLED IAW SR - [SDR CAL950803](https://openairdocs.org/sdr/CAL950803), Aug 27, 1995: LONGERON. CORRODED. HOU - INSPECTION FOUND CORROSION ON LONGERONS 26L TO 28L IN AFT BAGGAGE BIN BETWEEN STATION 937-945. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND R - [SDR CAL950805](https://openairdocs.org/sdr/CAL950805), Aug 24, 1995: RIB. CRACKED. HOU - INSPECTION FOUND THREE .25 INCH CRACKS IN WING LEADING EDGE RIB AT STATION XRS 501. A DOUBLER, FILLER, AND CLIP WERE FABRICATED AND INSTALLED IAW ECRA 572 - [SDR CAL950762](https://openairdocs.org/sdr/CAL950762), Aug 23, 1995: SKIN. CRACKED. HOU - INSPECTION FOUND A .5 INCH CRACK IN SKIN ON TOP SIDE OF NR 2 ENGINE PYLON. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-0 - [SDR CAL950497](https://openairdocs.org/sdr/CAL950497), Jun 17, 1995: PROX CONTROL BOX. INOPERATIVE. IAH - FLT 1536 - THE LEFT GEAR UNSAFE LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK AFTER DEPARTING IAH. CYCLING THE GEAR AND REPEATING THE UPLATCH CHECK GAVE - [SDR CAL950472](https://openairdocs.org/sdr/CAL950472), Jun 9, 1995: SEAL. FAILED. FLT NR 1781 - GSO - THE CABIN BEGAN TO FILL WITH SMOKE DURING TAXI OUT FOR DEPARTURE. THE AIRCRAFT BEGAN A RETURN TO THE GATE AND WAS ACCOMPANIED BY EMERGENCY V - [SDR CAL950338](https://openairdocs.org/sdr/CAL950338), Apr 27, 1995: S/O VALVE. LEAK. FLT NR 1581 - IAH - UPON LANDING FOUND HYDRAULIC FLUID LEAKING AT RUDDER. FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED SHUTOFF VALVE NO FURTHER ACTION. (W - [SDR CAL950153](https://openairdocs.org/sdr/CAL950153), Feb 26, 1995: BUNGEE CYL. INOPERATIVE. FLT NR 1647 - CLE - THE LEFT MLG RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND BOTH RED LIGHTS E - [SDR CAL950148](https://openairdocs.org/sdr/CAL950148), Feb 23, 1995: EEL BATT. DISCHARGED. JAX - FLT 1521 - THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE FWD OVERWING EMERGENCY EXIT LIGHT W ## Other aircraft with N14524 - [Registered now](https://openairdocs.org/aircraft/N14524): Airbus S A S A321-271NX, S/N 12061, built 2024 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.