# N835AT: 1971 Mcdonnell Douglas DC-9-32, registration cancelled 2005-01-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 19, 2005 - Exported to: Mexico - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47534 - Year built: 1971 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 25, 1995 - Certificate issued: November 3, 2004 - Last registry action: November 3, 2004 - Mode S code: AB6AFF - Owner when cancelled: [Aerofinance LLC](https://openairdocs.org/faa-owner/AEROFINANCE%20LLC) - Location: [Doral, FL](https://openairdocs.org/faa-place/FL/Doral) - Owner type: Corporation - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N835AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=835AT - Page: https://openairdocs.org/deregistered/N835AT-2005-01-19 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 (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT0200054](https://openairdocs.org/sdr/AT0200054), Mar 7, 2002: BULKHEAD. CORRODED. AFT PRESSURE BULKHEAD CORROSION FORWARD SIDE ABOVE 27L TO 27R. INSTALLED AFT PRESSURE BULKHEAD WEB REPAIR FROM LONG 28LT TO LONG 27RT IAW DC-9 SRM 53-03 FIG 33. - [SDR AT0200053](https://openairdocs.org/sdr/AT0200053), Feb 27, 2002: SKIN. CRACKED. RIGHT WING LEADING EDGE SKIN LOWER AREA CRACKED WING STA 215 XRS, JUST INBOARD FUEL PANEL DOOR. CUT OUT CRACK AREA, ACCOMPLISHED NDT CRACK CONTAINMENT CONFIRM. - [SDR AT0200052](https://openairdocs.org/sdr/AT0200052), Feb 27, 2002: SKIN. TORN. EXTERNAL FUSELAGE SKIN TORN AT LONGERON 18R APPROX STA 164. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER DC-9 SRM 53-04 FIG 12B CLASS II. - [SDR AT0000513](https://openairdocs.org/sdr/AT0000513), Dec 11, 2000: FITTING. CRACKED. FOUND RIGHT AFT KEEL BEAM FITTING CRACKED AT BS 738 - 756. REMOVED AND REPLACED FITTING ON RIGHT MLG WHEEL WELL, REMOVED AND REINSTALLED HYDRAULIC RESERVIOR AND - [SDR AT0000508](https://openairdocs.org/sdr/AT0000508), Dec 7, 2000: FLOOR SUPPORT. CRACKED. FOUND AFT CRAGO COMPARTMENT FRAME 813 LONGERON 29R CARGO FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT, WELD REPAIR FLOOR SUPPORT, REINSTALLED FLOOR SUPPORT IAW - [SDR AT0000511](https://openairdocs.org/sdr/AT0000511), Dec 6, 2000: PYLON. CRACKED. FOUND NR 2 ENGINE PYLON LOWER AND UPPER TRAILING EDGE PANEL HAS LOOSE AND MISSING FASTENERS. REMOVED AND REPLACED NR 2 ENGINE TRAILING EDGE PANEL UPPER AND LOWE - [SDR AT0000507](https://openairdocs.org/sdr/AT0000507), Dec 6, 2000: SPAR CAP. CORRODED. FOUND CORROSION ON FORWARD FLANGE OF LEFT HORIZONTAL UPPER REAR SPAR. REMOVED UPPER LEFT HAND HORIZONTAL SPAR CAP FROM SPAR CAP AT XRS 100. FORMED REPAIR ANGLE - [SDR AT0000512](https://openairdocs.org/sdr/AT0000512), Dec 5, 2000: SKIN. DAMAGED. FOUND AT BS 498R ONE STATIC DISCHARGE SPOT ON AFT SIDE OF WINDOW CUTOUT. REPAIRED STATIC DISCHARGE SPOT ON WINDOW CUTOUT IAW REO L00335. - [SDR AT0000509](https://openairdocs.org/sdr/AT0000509), Dec 5, 2000: TAIL CONE. CORRODED. FOUND VERTICAL STAB TAIL CONE HAS SURFACE CORROSION ON THE RIGHT AFT SIDE AND UNDER AFT SIDE. REMOVED CORROSION ON VERTICAL STAB. FABRICATED, TREATED AND INSTAL - [SDR AT0000510](https://openairdocs.org/sdr/AT0000510), Dec 4, 2000: SKIN. CORRODED. FOUND FUSELAGE SKIN BULGING AROUND FASTENERS AT BS 889 LONGERON 29R. REMOVED CORRODED SKIN, REMOVED AND REPLACED AFT CARGO DOOR FRAME INTERNAL DOUBLER, TREATED - [SDR AT0000361](https://openairdocs.org/sdr/AT0000361), Jul 25, 2000: SHUTOFF VALVE. CRACKED. RIGHT HYDRAULIC SYSTEM FAILED AND DURING TAXI, HYDRAULIC FUMES ENTERED THE CABIN. ALL PASSENGERS WERE EVACUATED VIA FORWARD STAIRS. FOUND RUDDER HYDRAULIC SHUTO - [SDR AT9900888](https://openairdocs.org/sdr/AT9900888), Dec 10, 1999: LAMP. FAILED. OVERHEAD EMERGENCY LIGHT AT L1 DOOR WOULD NOT ILLUMINATE. RELAMPED OVERHEAD EMERGENCY LIGHT IAW MM 33-50, OPS CHECK NORMAL. - [SDR AT9900716](https://openairdocs.org/sdr/AT9900716), Oct 9, 1999: FLOORBEAM. CORRODED. FOUND WEB AT BS 120, RBL 16 TO RBL 20 CORRODED, FORWARD AND AFT OF FLOORBEAM WAS BULDGED AND CRACKED. FABRICATED AND INSTALLED REPAIR WEBS AND 5 SPLICES IAW DC9 - [SDR AT9900715](https://openairdocs.org/sdr/AT9900715), Oct 7, 1999: JAMB. CRACKED. FOUND FORWARD COMPARTMENT LOWER DOOR JAMB CORNER CRACKED .5 INCH ON OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR IAW EO - [SDR AT9900796](https://openairdocs.org/sdr/AT9900796), Sep 29, 1999: DOUBLER. CORRODED. FOUND MILLED DOUBLERS CORRODED BEYOND LIMITS AT BS 340 LONGERON 30. REMOVED AND REPLACED WITH NEW DOUBLERS IAW DC9 SRM 51-10-3, 51-30-1, 51-30-2. - [SDR AT9900797](https://openairdocs.org/sdr/AT9900797), Sep 22, 1999: FUSELAGE SKIN. DENTED. FOUND RIGHT FUSELAGE SKIN DENTED OUT OF LIMITS AT BS 229-408. REMOVED AND REPLACED SKIN PANEL AT BS 229-408, LONG 18-26 IAW DC9 SRM 51-10-3, 51-10-2, 51-30-2, A - [SDR AT9900755](https://openairdocs.org/sdr/AT9900755), Sep 17, 1999: FLOOR SUPPORT. CORRODED. FOUND PANEL SUPPORT AT BS 200-238, LBL 13 CORRODED OUT OF LIMITS. REMOVED AND FABRICATED REPAIR SECTION ON SUPPORT. ALODINED AND PRIMED REPAIR. INSTALLED REPAIR - [SDR AT9900720](https://openairdocs.org/sdr/AT9900720), Sep 17, 1999: SUPPORT. CORRODED. FOUND PANEL SUPPORT AT BL 0 SB 160-218 WAS CORRODED. REMOVED CORRODED SUPPORT, FABRICATED NEW SUPPORT DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30- - [SDR AT9900677](https://openairdocs.org/sdr/AT9900677), Sep 17, 1999: TEE. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND COCKPIT MOUNTING TEE AT BS 160 WAS CORRODED. REMOVED, FABRICATED, AND INSTALLED FLOOR MOUNT SUPPO - [SDR AT9900695](https://openairdocs.org/sdr/AT9900695), Sep 10, 1999: LIGHT. CORRODED. FOUND RIGHT HAND LEADING EDGE LIGHT FIXTURE WAS CORRODED OUT OF LIMITS. REMOVED CORROSION INSIDE LIGHT FIXTURE, NET LOSS 80 PERCENT, FOUND TO BE OUT OF LIMITS. - [SDR AT9900731](https://openairdocs.org/sdr/AT9900731), Sep 9, 1999: FLOOR. CORRODED. FOUND FORWARD ENTRY FLOOR PANEL NR 4699 CHANNEL TIPS CHAFED, CORROSION AROUND NUT PLATES, AND CORROSION ON TOP AND BOTTOM SURFACES. FABRICATED NEW PANEL AND HAT - [SDR AT9900697](https://openairdocs.org/sdr/AT9900697), Sep 9, 1999: FLOOR. CORRODED. FOUND FLOOR PANEL UNDER 1ST OFFICERS SEAT CORRODED AT BS 120-131. FABRICATED NEW FLOOR PANEL AND HAT FRAMES. INSTALLED NEW HAT FRAMES AND FLOOR PANEL IAW DC9 SR - [SDR AT9900696](https://openairdocs.org/sdr/AT9900696), Sep 9, 1999: FLOOR. CRACKED. FOUND FLOOR PANEL AT FS 598 CRACKED AND CUT, 3 HAT CHANNELS CRACKED. FABRICATED NEW PANEL AND INSTALLED NEW HAT CHANNELS IAW DC9 SRM 51-10-1, 51-10-2, 51-10-4, - [SDR AT9900676](https://openairdocs.org/sdr/AT9900676), Sep 9, 1999: PANEL. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND SUBFLOOR PANEL WAS CORRODED AT LT CUSPLINE TO BS 0 AND RT CUSPLINE TO BS 160-218. REMOVED, FABRIC - [SDR AT9900727](https://openairdocs.org/sdr/AT9900727), Sep 8, 1999: FLOOR. CORRODED. FOUND FORWARD ENTRY FLOOR PANEL 4692B WAS CORRODED, 3 HAT SECTIONS LOOSE, AND GIL LINER STRIPS MISSING. FABRICATED NEW PANEL IAW DC9 SRM 53-21-0, 51-10-3, 51-30 - [SDR AT9900730](https://openairdocs.org/sdr/AT9900730), Sep 7, 1999: FLOOR. CORRODED. FOUND FORWARD ENTRY FLOOR PANEL NR 4698 WAS CORRODED AND HAD ELONGATED MOUNT HOLES. FABRICATED NEW PANEL IAW DC9 SRM 51-10-2, DPS3-40.9. - [SDR AT9900728](https://openairdocs.org/sdr/AT9900728), Sep 7, 1999: FLOOR. CORRODED. FOUND FLOOR PANEL 4697B CRACKED AND CORRODED. FABRICATED NEW PANEL IAW DC9 SRM 51-10-2 TO 51-30-2. - [SDR AT9900675](https://openairdocs.org/sdr/AT9900675), Sep 2, 1999: FLOOR. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FORWARD ENTRY FLOOR PANEL NR 894 WAS CORRODED. FABRICATED NEW SKIN FOR FLOOR PANEL NR 894 IAW DC9 - [SDR AT9900674](https://openairdocs.org/sdr/AT9900674), Sep 2, 1999: FLOOR. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FORWARD ENTRY FLOOR PANEL NR 4696 WAS CORRODED. FABRICATED NEW SKIN FOR FLOOR PANEL NR 4696 IAW D - [SDR AT9900726](https://openairdocs.org/sdr/AT9900726), Aug 27, 1999: FLOOR. CORRODED. FOUND FLIGHT DECK CENTER FLOOR PANEL CORRODED AT BS 160 LONG 30. FABRICATED FLOOR PANEL IAW DC9 SRM 51-10-2, 51-30-2. - [SDR AT9900729](https://openairdocs.org/sdr/AT9900729), Aug 8, 1999: FLOOR. CORRODED. FOUND FORWARD ENTRY FLOOR PANEL 4692 HAD 2 CRACKED CHANNELS, TWO CHANNELS LOOSE, AND CORROSION ON EDGE OF PANEL. FABRICATED NEW PANEL IAW DC9 SRM 53-21-0, 51-10 - [SDR AT9900499](https://openairdocs.org/sdr/AT9900499), Jul 23, 1999: PUMP. FAILED. LOSS RIGHT ENGINE HYDRAULIC PUMP INFLT FOLLOWED BY LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER M/M 29-10 - [SDR AT9900179](https://openairdocs.org/sdr/AT9900179), Mar 5, 1999: BATTERY. DISCHARGED. EMERGENCY LIGHTING AFT CABIN CEILING BY AFT DOOR DID NOT ILLUMINATED BRIGHTLY. CHARGED BATTERIES IAW 33-53-0, OPERATIONAL CHECK GOOD. - [SDR AT9900178](https://openairdocs.org/sdr/AT9900178), Mar 5, 1999: WIRE. OUT OF POSITION. EMERGENCY LIGHTING IN COCKPIT DID NOT ILLUMINATE. REPOSITIONED WIRING ON CONNECTOR IN FORWARD AISLE LIGHTING RECEPTICAL. OPERATIONAL CHECKS GOOD IAW DC9 STANDAR - [SDR AT9900035](https://openairdocs.org/sdr/AT9900035), Jan 1, 1999: SKIN. CHAFED. SCHEDULED INSPECTION AT AERO CORP, FL. RIGHT HAND AFT VERTICAL SKIN IS CHAFED. REMOVED AND REPLACED THE SKIN IAW DC9 SRM 55-32-0 FIG 7, 51-10-2, 51-10-3 AND RES ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20000725021729I](https://openairdocs.org/incident/20000725021729I), Jul 25, 2000: Doug DC932 (N835AT), Ft Lauderdale, FL. (-23)50 Miles west of fll, descending through 11K lost the rt hyd sys indications were rt hyd press low light on & quanity & press gages at zero. Procedures… ## Other aircraft with N835AT - [Registered now](https://openairdocs.org/aircraft/N835AT): Piper PA-44-180, S/N 4496315, built 2012 --- 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.