N839AT, cancelled Aug 16, 2013

Service difficulty reports · 87

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N839AT' AND deregistration_id = 'N839AT-2013-08-16'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AT0200066Slide · out of positionSLIDE PACK FELL OFF DOOR L1. REINSTALLED SLIDE PACK IAW MM 25-62.Jun 26, 2002 · N839AT · Doug DC932 · Escape SlideSDR AT0200032Skin · crackedFUSELAGE SKIN IS CRACKED AT THE FORWARD PASSENGER DOOR CUTOUT AT THE NR 1 AFT DOOR STOP.Feb 2, 2002 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0200035LongeronLONG. 8R CRACKED AT STATION 718. CORRECTIVE ACTION: INSTALLED LONGERON REPAIR AT STATION 718 L-8R IN ACCORDANCE WITH DC-9 SRM 53-02, FIGURE 18. MATERIAL USED LONGERON (SPLICE) P/N 52777922-4-12000, LONGERON P/N 7637813-3,LOT # 1WOWGBH3, P.O. # : 2KJan 31, 2002 · N839AT · Doug DC932 · Fuselage Main, StructureSDR AT0200034Window Frame · damagedCABIN WINDOW FRAME 33 RIGHT THIN SPOT, EXTERIOR RIM.Jan 28, 2002 · N839AT · Doug DC932 · Passenger Compartment WindowsSDR AT0200033Bulkhead · crackedCOMPLIED WITH AD PER SERVICE BULLETIN , X-RAY, AND CRACKS NOTED ON FILMS, AFT PRESSURE BULKHEAD 2 EA CRACKS UPPER RIGHT SIDE.Jan 26, 2002 · N839AT · Doug DC932 · Fuselage Main, BulkheadSDR AT0100121Coalescer Bag · dirtyAIRCRAFT HAD CHEMICAL SMELL AND AFT LEFT SMOKE DETECTORS SOUNDED. REPLACED BOTH COALESCER BAGS AND RAN ENGINES.Mar 28, 2001 · N839AT · Doug DC932 · Humidity Control SystemSDR AT0100042R1Pan · corrodedFOUND C2 DOOR LOWER PAN CORRODED BEYOND LIMITS. REPLACED LOWER PAN IAW DC9 SRM 53-04 FIG 44, 51-10-03, 51-10-04, 51-30-02, AND 51-30-05.Jan 19, 2001 · N839AT · Doug DC932 · Fuselage Main, StructureSDR AT0100032R1Spar · corrodedFOUND RIGHT WING REAR SPAR TO HAVE INTERGRANULAR EXFOLIATED CORROSION INBOARD OF CENTER FLAP SUPPORT FITTING. REMOVED CORROSION AND FABRICATED AND INSTALLED SPLICES IAW REO-L00303.Jan 11, 2001 · N839AT · Doug DC932 · Wing SparSDR AT0100033R1Floorboard · corrodedFOUND FORWARD ENTRY FLOORBOARD 4693 CORRODED BEYOND LIMITS. REPLACED FLOORBOARD IAW DC9 SRM 53-01 FIG 1, 51-10-02, 51-10-04, 51-30-03, 51-10-03, AND 51-30-01.Jan 1, 2001 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0000505Door · openLOUD VIBRATION AFTER TAKE OFF RETURNED WITH ENEVENTFUL OVERWEIGHT LANDING, FOUND NOSE GEAR DOORS OPEN. PERFORMED OVERWEIGHT INSPECTION, CLOSED NOSE GEAR DOORS. IAW 5-15-0 PAGE 602, 603, 607 A INSPECTION.Dec 21, 2000 · N839AT · Doug DC932 · Landing Gear DoorsSDR AT0100027Spar · corrodedFOUND RIGHT HORIZONTAL STABILIZER FORWARD SPAR XFS 161-163 EXFOLIATED CORROSION. FABRICATED AND INSTALLED FILLER AND NUT PLATE STRIP IAW REO-L00320.Nov 22, 2000 · N839AT · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR AT0100022Floor Panel · corrodedFOUND COCKPIT FLOORPANEL 4416 CORRODED BEYOND LIMITS. REPLACED SKIN ON FLOOR PANEL 4416 IAW DC9 SRM 53-01, 53-21, AND 51-10-03.Nov 22, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100031Skin · chafedFOUND CHAFE MARKS OUT OF LIMITS IN VERTICAL STABILIZER LEADING EDGE. REPLACED LEADING EDGE OF VERTICAL STABILIZER IAW DC9 SRM 55-01 FIG 1.Nov 17, 2000 · N839AT · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR AT0100038Stringer · corrodedFOUND RIGHT WING XCW 58.5 STRINGER 13 CORRODED. INSTALLED STRINGER 13 SPLICES IAW EO 4-5740-29-E1549 .Nov 16, 2000 · N839AT · Doug DC932 · Wing, Longeron/StringerSDR AT0100030Floorboard · gougedFOUND FLOORBOARD 96C HAS GOUGE OUT OF LIMITS. REPLACED FLOORBOARD SKIN IAW DC9 SRM 53-01 FIG 1, 53-21, 51-10-04, 51-10-03, 51-30, AND 51-30-02.Nov 16, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100037Floorboard · corrodedFOUND SURFACE CORROSION ON SERVICE DOOR ENTRY FLOORBOARD. INSTALLED NEW SKIN IAW DC9 SRM 51-10-04, 51-10-02, AND 51-10-03.Nov 15, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100023Intercostal · corrodedFOUND INTERCOSTAL CORRODED BEYOND LIMITS AT BS 962 LONGERON 18R. FORMED AND INSTALLED REPAIR IAW DC9 SRM 52-11-03, 51-10-02, 51-30-01, 51-30-02, AND 51-20-05.Nov 8, 2000 · N839AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100039Floorbeam · corrodedFOUND FLOOR SUPPORT BEAM AT BS 996 RBL 55-21 CORRODED BEYOND LIMITS. REPLACED FLOORBEAM CAP IAW 51-10-04, 51-30-02, AND 53-01 FIG 1.Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0100036Floorboard · corrodedFOUND FORWARD ENTRY FLOORBOARD 4691 CORRODED BEYOND LIMITS. REPLACED FLOORBOARD SKIN IAW DC9 SRM 51-10-02, 51-30-02, AND 51-20-10.Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100035Floorboard · corrodedFOUND FLOORBOARD 4695 CORRODED BEYOND LIMITS. REPLACED FLOORBOARD SKIN IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30-02, AND 53-20-03.Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100034Floorboard · corrodedFOUND COCKPIT CENTER FLOORPANEL CORRODED BEYOND LIMITS. REPLACED FLOORBOARD SKIN IAW DC9 SRM 51-30-02 AND 51-30-01.Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100028Doubler · corrodedFOUND R-1 DOOR DOUBLER CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-02, 53-21 FIG 2E, 51-10-04, AND 51-10-03.Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0100025Static Wick · corrodedFOUND RIGHT ELEVATOR CORRODED AROUND STATIC WICK BASE. REPLACED STATIC WICK AND BASE FROM RIGHT ELEVATOR IAW DC9 SRM 51-10-04, 51-10-03, 51-30-08, 51-20, AND 51-30-02.Nov 7, 2000 · N839AT · Doug DC932 · Static Discharge SystemSDR AT0100018Skin · chafedFOUND CHAFE AT LEFT WING NR 5 LEADING EDGE SLAT. BLENDED CHAFED AREA IAW REO-L00322.Nov 7, 2000 · N839AT · Doug DC932 · Leading Edge DevicesSDR AT0100029Panel · lightning strikeFOUND LIGHTNING STRIKE AT BS 421, 8 INCHES ABOVE LONGERON 15L OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 111A, 56-20, AND 25-21.Nov 5, 2000 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0100026Skin · lightning strikeFOUND LIGHTNING STRIKE AT BS 605 6 INCHES BELOW LONGERON 11L OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111A AND REO-L00324.Nov 5, 2000 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0100024Bulkhead · crackedFOUND CRACK IN UPPER BULKHEAD BS 94.55. DRILLED STOP CRACK AND INSTALLED INTERNAL AND EXTERNAL DOUBLER IAW SB 53-187 REV 2.Nov 5, 2000 · N839AT · Doug DC932 · Fuselage Main, BulkheadSDR AT0100033Floorboard · corrodedFOUND FORWARD ENTRY FLOORBOARD 4693 CORRODED BEYOND LIMITS. REPLACED FLOORBOARD IAW DC9 SRM 53-01 FIG 1, 51-10-02, 51-10-04, 51-30-03, 51-10-03, AND 51-30-01.Nov 1, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT0100032Spar · corrodedFOUND RIGHT WING REAR SPAR TO HAVE INTERGRANULAR EXFOLIATED CORROSION INBOARD OF CENTER FLAP SUPPORT FITTING. REMOVED CORROSION AND FABRICATED AND INSTALLED SPLICES IAW REO-L00303.Nov 1, 2000 · N839AT · Doug DC932 · Wing SparSDR AT0000173Light · inoperativeFOUND EMERGENCY LIGHTS INOPERATIVE ABOVE AFT EVACUATION SLIDE. CORRECTIVE ACTION: RELAMPED IAW DC9 MM.Apr 6, 2000 · N839AT · Doug DC932 · Emergency LightingSDR AT0000172Light · inoperativeFOUND EMERGENCY LIGHTS OUT IN VENTRAL STAIR AREA. CORRECTIVE ACTION: REPLACED BATTERY PACKS IAW DC9 MM.Apr 6, 2000 · N839AT · Doug DC932 · Emergency LightingSDR AT0000143Floorbeam · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR SUPPORT CORRODED ON BOTH SIDES AT BS 200, RBL 44 - 56. CORRECTIVE ACTION: FABRICATED AND INSTALLED NEW SUPPORT IAW DC SRM53-01 FIG 1, 51-10-02, AND 51-10-03.Mar 15, 2000 · N839AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0000112Latch · looseAIRCRAFT RETURNED FROM FLIGHT DUE TO UNSAFE GEAR UP INDICATION. TIGHTENED LEFT GEAR DOOR LATCH IAW DC9 MM.Mar 1, 2000 · N839AT · Doug DC932 · Landing Gear DoorsSDR AT0000014Glide Slope · inoperativeATTEMPTED 3 APPROACHES INTO ATLANTA (ATL), BOTH NAV'S FAILED ON ALL THREE APPROACHES, CONDITIONS WERE ILS. AIRCRAFT DIVERTED TO (AGS) AUGUSTA FOR A VFR APPROACH. REMOVED AND REPLACED BOTH NAV RECEIVERS IAW DC9 MM 34-00.Jan 10, 2000 · N839AT · Doug DC932 · Glide Slope SystemSDR AT9900743Hose · out of positionDURING CLIMBOUT, THE GEAR DOOR OPEN LIGHT ILLUMINATED. RIGHT HYDRAULIC OVERFLOW BOTTLE HOSE WAS FOUND STUCK IN DOOR. REPOSITIONED DRAIN HOSE FOR CLEARANCE.Oct 24, 1999 · N839AT · Doug DC932 · Hydraulic System, MainSDR ATT9900673Switch · failedSHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO OIL QUANTITY LOSS. FOUND OIL PRESSURE SWITCH DISINTEGRATED.Sep 27, 1999 · N839AT · Doug DC932 · Engine Oil PressureSDR AT9900673R1Switch · malfunctionedSHUT DOWN NR 2 ENGINE IN FLIGHT DUE TO OIL QUANTITY LOSS. FOUND OIL PRESSURE SWITCH DISINTEGRATED. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SWITCH AND LOW OIL PRESSURE SWITCH IAW MM 79-32.Sep 27, 1999 · N839AT · Doug DC932 · Engine Oil Indicating SystemSDR AT9900670Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND THE SKIN PANEL AT BS 332 - 362 L18R TO L26R CORRODED. A CLASS II TEMP REPAIR INSTALLED IN THE AREA. REMOVED SKIN, FABRICATED AND INSTALLED SKIN REPAIR IAW EO 99-123-9.Sep 18, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900644Floor · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND THE RIGHT SIDE CABIN FLOOR PANEL AT BS 200-237 CORRODED. FABRICATED NEW PANELS AND INSTALLED NEW HAT CHANNELS IAW DC9 SRM 53-05, 51-10-04, 51-10-03, 51-30-02, 53-21-0.Sep 18, 1999 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT9900667Angle · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LEFT HAND AND RIGHT HAND OUTBOARD SUPPORT ANGLES FOR THE AIR STAIRS, 4TH STEP FROM THE TOP CORRODED. REMOVED, FABRICATED AND INSTALLED 2 SUPPORT ANGLES IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-1 ASep 14, 1999 · N839AT · Doug DC932 · Entrance StairsSDR AT9900658Step · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND AFT VENTRAL STAIRS 5TH STEP FROM TOP. VERTICAL RISER ON STEP CORRODED. REMOVED AND REPLACED STEP IAW DC9 SRM 51-30-1, 52-01 FIGURE 1.Sep 12, 1999 · N839AT · Doug DC932 · Entrance StairsSDR AT9900671Support · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND THE AFT VENTRAL STAIRWAY CENTER HANDRAIL SUPPORT CORRODED. REMOVED AND REPLACED HANDRAIL SUPPORT IAW DC9 SRM 52-63-0.Sep 10, 1999 · N839AT · Doug DC932 · Entrance StairsSDR AT9900668Intercostal · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND AFT AIR STAIRS STEP NR 6 INTERCOSTAL CORRODED. FABRICATED AND INSTALLED REPAIR INTERCOSTAL SUPPORT IAW DC9 SRM 51-10-2, 51-10-2A, 51-30-1, 51-30-2, 51-30-5.Sep 10, 1999 · N839AT · Doug DC932 · Entrance StairsSDR AT9900657Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LOWER FUSELAGE SKIN BULGED AT LONGERON 30 BS 605-654. FABRICATED AND INSTALLED EXTERNAL REPAIR IAW DC9 SRM 53-01, FIGURE 2, 51-30-1, 51-10-3.Sep 9, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900656Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LOWER FUSELAGE SKIN BULGED AT BS 609 AND L30L. REMOVED AND REPLACED END FITTINGS AND REPAIRED T CHORDS ON L28L AND L30L IAW DC9 SRM 53-03, FIGURE 10.Sep 8, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900654Skin · dentedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND DENT AT BS 210. FABRICATED AND INSTALLED REPAIR DOUBLER IAW TIMCO RES NR 07634 AND DC9 SRM 53-04.Sep 8, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900665Floor · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND FLOOR PANEL AT REAR OF COCKPIT, BETWEEN ELECTRICAL PANEL AND RIGHT SIDE WALL CORRODED. REMOVED, FABRICATED NEW SKIN. INSTALLED CHANNELS ON SKIN AND INSTALLED PANEL IAW DC9 SRM 51-10-3, 51-10-4, 51-30Sep 7, 1999 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT9900664Floor · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND RT OUTER FLOOR PANEL NR 40 HAS ELONGATED HOLES AND CORROSION. FABRICATED NEW FLOOR PANEL IAW DC9 SRM 51-30-21, 51-10-2/-3/-4.Sep 7, 1999 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT9900662Floor · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND RT OUTER FLOOR PANEL NR 39 HAS ELONGATED HOLES AND CORROSION. FABRICATED NEW FLOOR PANEL SKIN AND REINSTALLED HAT CHANNELS IAW DC9 SRM 53-21-0, 51-70-3.Sep 7, 1999 · N839AT · Doug DC932 · Fuselage Floor PanelSDR AT9900666Cusp · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION AT LOWER EDGE FORWARD SERVICE DOOR CUTOUT BETWEEN SKIN AND DOUBLER. REMOVED AND REPLACED R1 DOOR CUSP IAW DC9 SRM 53-05 FIGURE 55, 51-30-1, 51-30-5.Sep 5, 1999 · N839AT · Doug DC932 · Fuselage Miscellaneous Structure
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