# Service difficulty reports: N835AT, cancelled Jan 19, 2005 A list on [N835AT, cancelled Jan 19, 2005](https://openairdocs.org/deregistered/N835AT-2005-01-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT0200054](https://openairdocs.org/sdr/AT0200054.md): Bulkhead · corroded · Mar 7, 2002 · N835AT · Doug DC932 · Fuselage Main, Bulkhead > 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.md): Skin · cracked · Feb 27, 2002 · N835AT · Doug DC932 · Wing, Plate/Skin > 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. INSTALLED REPAIR PER DC-9 SRM 57-06B F1. - [SDR AT0200052](https://openairdocs.org/sdr/AT0200052.md): Skin · torn · Feb 27, 2002 · N835AT · Doug DC932 · Fuselage Main, Plate/Skin > 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.md): Fitting · cracked · Dec 11, 2000 · N835AT · Doug DC932 · Fuselage Main, Keel > 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 HYDRAULIC LINES IAW DC9 MM 29-00-01 AND SRM 51-10-6, 51-30-1. - [SDR AT0000508](https://openairdocs.org/sdr/AT0000508.md): Floor Support · cracked · Dec 7, 2000 · N835AT · Doug DC932 · Fuselage Miscellaneous Structure > FOUND AFT CRAGO COMPARTMENT FRAME 813 LONGERON 29R CARGO FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT, WELD REPAIR FLOOR SUPPORT, REINSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-4, 51-30-2, EA 12-5321-29-C1362, 51-30-2, 51-30-5. - [SDR AT0000511](https://openairdocs.org/sdr/AT0000511.md): Pylon · cracked · Dec 6, 2000 · N835AT · Doug DC932 · Nacelle/Pylon, Plate/Skin > 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 LOWER SKINS. REMOVED AND REPLACED WEDGE, REMOVED AND REINSTALLED NR 2 ENGINE PYLON TRAILING EDGE ASSEM - [SDR AT0000507](https://openairdocs.org/sdr/AT0000507.md): Spar Cap · corroded · Dec 6, 2000 · N835AT · Doug DC932 · Horizontal Stabilizer, Spar/Rib > 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 AND SPLICES, HEAT TREATED, DRILLED, PRIMED AND INSTALLED IAW DC9 SRM 55-02 FIGURE 21, 51-30-2, 51- - [SDR AT0000512](https://openairdocs.org/sdr/AT0000512.md): Skin · damaged · Dec 5, 2000 · N835AT · Doug DC932 · Fuselage Main, Plate/Skin > 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.md): Tail Cone · corroded · Dec 5, 2000 · N835AT · Doug DC932 · Aerodynamic Fairings > 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 INSTALLED DOUBLER IAW DC9 51-10-3, 51-30-1, 51-10-4. - [SDR AT0000510](https://openairdocs.org/sdr/AT0000510.md): Skin · corroded · Dec 4, 2000 · N835AT · Doug DC932 · Fuselage Main, Plate/Skin > FOUND FUSELAGE SKIN BULGING AROUND FASTENERS AT BS 889 LONGERON 29R. REMOVED CORRODED SKIN, REMOVED AND REPLACED AFT CARGO DOOR FRAME INTERNAL DOUBLER, TREATED AND INSTALLED REPLACEMENT SKIN IAW REO L00337, DC9 SRM 53-04 FIGURE C12, 51-10-4, 51-10-3, 51-30-2, - [SDR AT0000361](https://openairdocs.org/sdr/AT0000361.md): Shutoff Valve · cracked · Jul 25, 2000 · N835AT · Doug DC932 · Hydraulic System, Main > RIGHT HYDRAULIC SYSTEM FAILED AND DURING TAXI, HYDRAULIC FUMES ENTERED THE CABIN. ALL PASSENGERS WERE EVACUATED VIA FORWARD STAIRS. FOUND RUDDER HYDRAULIC SHUTOFF VALVE CRACKED. - [SDR AT9900888](https://openairdocs.org/sdr/AT9900888.md): Lamp · failed · Dec 10, 1999 · N835AT · Doug DC932 · Emergency Lighting > 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.md): Floorbeam · corroded · Oct 9, 1999 · N835AT · Doug DC932 · Fuselage Main, Floor Beam > 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 SRM 51-10-3, 51-10-4, 51-30-1, 51-30-2, 51-30-5, 53-20-1, 27-20-2, 27-10-0. - [SDR AT9900715](https://openairdocs.org/sdr/AT9900715.md): Jamb · cracked · Oct 7, 1999 · N835AT · Doug DC932 · Fuselage Miscellaneous Structure > 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 99-1262, DC9 SRM 51-10-3, 51-30-2, 51-20-0, 51-30-0. - [SDR AT9900796](https://openairdocs.org/sdr/AT9900796.md): Doubler · corroded · Sep 29, 1999 · N835AT · Doug DC932 · Fuselage Miscellaneous Structure > 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.md): Fuselage Skin · dented · Sep 22, 1999 · N835AT · Doug DC932 · Fuselage Main, Plate/Skin > 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, AND TIMCO EO 99-1258 APPROVED BY 8110-3. - [SDR AT9900755](https://openairdocs.org/sdr/AT9900755.md): Floor Support · corroded · Sep 17, 1999 · N835AT · Doug DC932 · Fuselage Main, Floor Beam > 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 SECTION IAW DC9 SRM 51-30-2, 51-10-3, 53-01 FIGURE 2. - [SDR AT9900720](https://openairdocs.org/sdr/AT9900720.md): Support · corroded · Sep 17, 1999 · N835AT · Doug DC932 · Fuselage Miscellaneous Structure > 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 51-30-2, 51-10-2, 51-30-5. - [SDR AT9900677](https://openairdocs.org/sdr/AT9900677.md): Tee · corroded · Sep 17, 1999 · N835AT · Doug DC932 · Fuselage Miscellaneous Structure > 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 SUPPORT IAW DC9 SRM 51-30-1, 51-30-2, 53-11-1, 51-10-1, 51-10-2, 51-10-4, 53-01 FIGURE 2, 51-30-2, 51-30 - [SDR AT9900695](https://openairdocs.org/sdr/AT9900695.md): Light · corroded · Sep 10, 1999 · N835AT · Doug DC932 · Exterior Lighting > 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. REMOVED AND REPLACED LIGHT FIXTURE IAW DC SRM 51-10-3, 51-10-4, 51-30-2. - [SDR AT9900731](https://openairdocs.org/sdr/AT9900731.md): Floor · corroded · Sep 9, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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 SECTIONS IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2, 53-21-0. - [SDR AT9900697](https://openairdocs.org/sdr/AT9900697.md): Floor · corroded · Sep 9, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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 SRM 53-05 FIGURE 1, 51-30-2. - [SDR AT9900696](https://openairdocs.org/sdr/AT9900696.md): Floor · cracked · Sep 9, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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, 51-10-3, 51-30-2. - [SDR AT9900676](https://openairdocs.org/sdr/AT9900676.md): Panel · corroded · Sep 9, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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, FABRICATED, AND INSTALLED 3 EACH SUBFLOOR PANELS AT BS 160-218 IAW DC9 SRM 51-30-2, 53-30-2, 51-30-5, 51- - [SDR AT9900727](https://openairdocs.org/sdr/AT9900727.md): Floor · corroded · Sep 8, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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, 51-30-2. - [SDR AT9900730](https://openairdocs.org/sdr/AT9900730.md): Floor · corroded · Sep 7, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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.md): Floor · corroded · Sep 7, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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.md): Floor · corroded · Sep 2, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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 SRM 51-10-3, 51-30-2. - [SDR AT9900674](https://openairdocs.org/sdr/AT9900674.md): Floor · corroded · Sep 2, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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 DC9 SRM 51-10-3, 51-30-2. - [SDR AT9900726](https://openairdocs.org/sdr/AT9900726.md): Floor · corroded · Aug 27, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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.md): Floor · corroded · Aug 8, 1999 · N835AT · Doug DC932 · Fuselage Floor Panel > 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, 51-10-3, 51-30-2. - [SDR AT9900499](https://openairdocs.org/sdr/AT9900499.md): Pump · failed · Jul 23, 1999 · N835AT · Doug DC932 · Hydraulic Pump (Electric/Engine), Main > 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 29-10-5. RESERVICED RIGHT HYDRAULIC RESERVOIR AND INSTALLED TEMPORARY FLEX LINE ABOVE RIGHT THRUST REVE - [SDR AT9900179](https://openairdocs.org/sdr/AT9900179.md): Battery · discharged · Mar 5, 1999 · N835AT · Doug DC932 · Emergency Lighting > 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.md): Wire · out of position · Mar 5, 1999 · N835AT · Doug DC932 · Light System Wiring > EMERGENCY LIGHTING IN COCKPIT DID NOT ILLUMINATE. REPOSITIONED WIRING ON CONNECTOR IN FORWARD AISLE LIGHTING RECEPTICAL. OPERATIONAL CHECKS GOOD IAW DC9 STANDARD PRACTICES CHAPTER 20-50. - [SDR AT9900035](https://openairdocs.org/sdr/AT9900035.md): Skin · chafed · Jan 1, 1999 · N835AT · Doug DC932 · Vertical Stabilizer, Plate/Skin > 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 NR 982300. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N835AT' AND deregistration_id = 'N835AT-2005-01-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N835AT-2005-01-19/reports --- 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.