# Service difficulty reports: N839AT, cancelled Aug 16, 2013

A list on [N839AT, cancelled Aug 16, 2013](https://openairdocs.org/deregistered/N839AT-2013-08-16.md).

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

Page 1 of 2 · 87 reports

- [SDR AT0200066](https://openairdocs.org/sdr/AT0200066.md): Slide · out of position · Jun 26, 2002 · N839AT · Doug DC932 · Escape Slide
  > SLIDE PACK FELL OFF DOOR L1. REINSTALLED SLIDE PACK IAW MM 25-62.
- [SDR AT0200032](https://openairdocs.org/sdr/AT0200032.md): Skin · cracked · Feb 2, 2002 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS CRACKED AT THE FORWARD PASSENGER DOOR CUTOUT AT THE NR 1 AFT DOOR STOP.
- [SDR AT0200035](https://openairdocs.org/sdr/AT0200035.md): Longeron · Jan 31, 2002 · N839AT · Doug DC932 · Fuselage Main, Structure
  > LONG. 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. #: 2K
- [SDR AT0200034](https://openairdocs.org/sdr/AT0200034.md): Window Frame · damaged · Jan 28, 2002 · N839AT · Doug DC932 · Passenger Compartment Windows
  > CABIN WINDOW FRAME 33 RIGHT THIN SPOT, EXTERIOR RIM.
- [SDR AT0200033](https://openairdocs.org/sdr/AT0200033.md): Bulkhead · cracked · Jan 26, 2002 · N839AT · Doug DC932 · Fuselage Main, Bulkhead
  > COMPLIED WITH AD PER SERVICE BULLETIN, X-RAY, AND CRACKS NOTED ON FILMS, AFT PRESSURE BULKHEAD 2 EA CRACKS UPPER RIGHT SIDE.
- [SDR AT0100121](https://openairdocs.org/sdr/AT0100121.md): Coalescer Bag · dirty · Mar 28, 2001 · N839AT · Doug DC932 · Humidity Control System
  > AIRCRAFT HAD CHEMICAL SMELL AND AFT LEFT SMOKE DETECTORS SOUNDED. REPLACED BOTH COALESCER BAGS AND RAN ENGINES.
- [SDR AT0100042R1](https://openairdocs.org/sdr/AT0100042R1.md): Pan · corroded · Jan 19, 2001 · N839AT · Doug DC932 · Fuselage Main, Structure
  > FOUND 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.
- [SDR AT0100032R1](https://openairdocs.org/sdr/AT0100032R1.md): Spar · corroded · Jan 11, 2001 · N839AT · Doug DC932 · Wing Spar
  > FOUND 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.
- [SDR AT0100033R1](https://openairdocs.org/sdr/AT0100033R1.md): Floorboard · corroded · Jan 1, 2001 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND 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.
- [SDR AT0000505](https://openairdocs.org/sdr/AT0000505.md): Door · open · Dec 21, 2000 · N839AT · Doug DC932 · Landing Gear Doors
  > LOUD 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.
- [SDR AT0100027](https://openairdocs.org/sdr/AT0100027.md): Spar · corroded · Nov 22, 2000 · N839AT · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > FOUND RIGHT HORIZONTAL STABILIZER FORWARD SPAR XFS 161-163 EXFOLIATED CORROSION. FABRICATED AND INSTALLED FILLER AND NUT PLATE STRIP IAW REO-L00320.
- [SDR AT0100022](https://openairdocs.org/sdr/AT0100022.md): Floor Panel · corroded · Nov 22, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND COCKPIT FLOORPANEL 4416 CORRODED BEYOND LIMITS. REPLACED SKIN ON FLOOR PANEL 4416 IAW DC9 SRM 53-01, 53-21, AND 51-10-03.
- [SDR AT0100031](https://openairdocs.org/sdr/AT0100031.md): Skin · chafed · Nov 17, 2000 · N839AT · Doug DC932 · Vertical Stabilizer, Plate/Skin
  > FOUND CHAFE MARKS OUT OF LIMITS IN VERTICAL STABILIZER LEADING EDGE. REPLACED LEADING EDGE OF VERTICAL STABILIZER IAW DC9 SRM 55-01 FIG 1.
- [SDR AT0100038](https://openairdocs.org/sdr/AT0100038.md): Stringer · corroded · Nov 16, 2000 · N839AT · Doug DC932 · Wing, Longeron/Stringer
  > FOUND RIGHT WING XCW 58.5 STRINGER 13 CORRODED. INSTALLED STRINGER 13 SPLICES IAW EO 4-5740-29-E1549.
- [SDR AT0100030](https://openairdocs.org/sdr/AT0100030.md): Floorboard · gouged · Nov 16, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND 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.
- [SDR AT0100037](https://openairdocs.org/sdr/AT0100037.md): Floorboard · corroded · Nov 15, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND SURFACE CORROSION ON SERVICE DOOR ENTRY FLOORBOARD. INSTALLED NEW SKIN IAW DC9 SRM 51-10-04, 51-10-02, AND 51-10-03.
- [SDR AT0100023](https://openairdocs.org/sdr/AT0100023.md): Intercostal · corroded · Nov 8, 2000 · N839AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR AT0100039](https://openairdocs.org/sdr/AT0100039.md): Floorbeam · corroded · Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR AT0100036](https://openairdocs.org/sdr/AT0100036.md): Floorboard · corroded · Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND FORWARD ENTRY FLOORBOARD 4691 CORRODED BEYOND LIMITS. REPLACED FLOORBOARD SKIN IAW DC9 SRM 51-10-02, 51-30-02, AND 51-20-10.
- [SDR AT0100035](https://openairdocs.org/sdr/AT0100035.md): Floorboard · corroded · Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND 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.
- [SDR AT0100034](https://openairdocs.org/sdr/AT0100034.md): Floorboard · corroded · Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND COCKPIT CENTER FLOORPANEL CORRODED BEYOND LIMITS. REPLACED FLOORBOARD SKIN IAW DC9 SRM 51-30-02 AND 51-30-01.
- [SDR AT0100028](https://openairdocs.org/sdr/AT0100028.md): Doubler · corroded · Nov 7, 2000 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND 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.
- [SDR AT0100025](https://openairdocs.org/sdr/AT0100025.md): Static Wick · corroded · Nov 7, 2000 · N839AT · Doug DC932 · Static Discharge System
  > FOUND 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.
- [SDR AT0100018](https://openairdocs.org/sdr/AT0100018.md): Skin · chafed · Nov 7, 2000 · N839AT · Doug DC932 · Leading Edge Devices
  > FOUND CHAFE AT LEFT WING NR 5 LEADING EDGE SLAT. BLENDED CHAFED AREA IAW REO-L00322.
- [SDR AT0100029](https://openairdocs.org/sdr/AT0100029.md): Panel · lightning strike · Nov 5, 2000 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND 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.
- [SDR AT0100026](https://openairdocs.org/sdr/AT0100026.md): Skin · lightning strike · Nov 5, 2000 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND 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.
- [SDR AT0100024](https://openairdocs.org/sdr/AT0100024.md): Bulkhead · cracked · Nov 5, 2000 · N839AT · Doug DC932 · Fuselage Main, Bulkhead
  > FOUND CRACK IN UPPER BULKHEAD BS 94.55. DRILLED STOP CRACK AND INSTALLED INTERNAL AND EXTERNAL DOUBLER IAW SB 53-187 REV 2.
- [SDR AT0100033](https://openairdocs.org/sdr/AT0100033.md): Floorboard · corroded · Nov 1, 2000 · N839AT · Doug DC932 · Fuselage Floor Panel
  > FOUND 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.
- [SDR AT0100032](https://openairdocs.org/sdr/AT0100032.md): Spar · corroded · Nov 1, 2000 · N839AT · Doug DC932 · Wing Spar
  > FOUND 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.
- [SDR AT0000173](https://openairdocs.org/sdr/AT0000173.md): Light · inoperative · Apr 6, 2000 · N839AT · Doug DC932 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS INOPERATIVE ABOVE AFT EVACUATION SLIDE. CORRECTIVE ACTION: RELAMPED IAW DC9 MM.
- [SDR AT0000172](https://openairdocs.org/sdr/AT0000172.md): Light · inoperative · Apr 6, 2000 · N839AT · Doug DC932 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS OUT IN VENTRAL STAIR AREA. CORRECTIVE ACTION: REPLACED BATTERY PACKS IAW DC9 MM.
- [SDR AT0000143](https://openairdocs.org/sdr/AT0000143.md): Floorbeam · corroded · Mar 15, 2000 · N839AT · Doug DC932 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR AT0000112](https://openairdocs.org/sdr/AT0000112.md): Latch · loose · Mar 1, 2000 · N839AT · Doug DC932 · Landing Gear Doors
  > AIRCRAFT RETURNED FROM FLIGHT DUE TO UNSAFE GEAR UP INDICATION. TIGHTENED LEFT GEAR DOOR LATCH IAW DC9 MM.
- [SDR AT0000014](https://openairdocs.org/sdr/AT0000014.md): Glide Slope · inoperative · Jan 10, 2000 · N839AT · Doug DC932 · Glide Slope System
  > ATTEMPTED 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.
- [SDR AT9900743](https://openairdocs.org/sdr/AT9900743.md): Hose · out of position · Oct 24, 1999 · N839AT · Doug DC932 · Hydraulic System, Main
  > DURING CLIMBOUT, THE GEAR DOOR OPEN LIGHT ILLUMINATED. RIGHT HYDRAULIC OVERFLOW BOTTLE HOSE WAS FOUND STUCK IN DOOR. REPOSITIONED DRAIN HOSE FOR CLEARANCE.
- [SDR ATT9900673](https://openairdocs.org/sdr/ATT9900673.md): Switch · failed · Sep 27, 1999 · N839AT · Doug DC932 · Engine Oil Pressure
  > SHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO OIL QUANTITY LOSS. FOUND OIL PRESSURE SWITCH DISINTEGRATED.
- [SDR AT9900673R1](https://openairdocs.org/sdr/AT9900673R1.md): Switch · malfunctioned · Sep 27, 1999 · N839AT · Doug DC932 · Engine Oil Indicating System
  > SHUT 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.
- [SDR AT9900670](https://openairdocs.org/sdr/AT9900670.md): Skin · corroded · Sep 18, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR AT9900644](https://openairdocs.org/sdr/AT9900644.md): Floor · corroded · Sep 18, 1999 · N839AT · Doug DC932 · Fuselage Floor Panel
  > DURING 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.
- [SDR AT9900667](https://openairdocs.org/sdr/AT9900667.md): Angle · corroded · Sep 14, 1999 · N839AT · Doug DC932 · Entrance Stairs
  > DURING 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 A
- [SDR AT9900658](https://openairdocs.org/sdr/AT9900658.md): Step · corroded · Sep 12, 1999 · N839AT · Doug DC932 · Entrance Stairs
  > DURING 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.
- [SDR AT9900671](https://openairdocs.org/sdr/AT9900671.md): Support · corroded · Sep 10, 1999 · N839AT · Doug DC932 · Entrance Stairs
  > DURING 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.
- [SDR AT9900668](https://openairdocs.org/sdr/AT9900668.md): Intercostal · corroded · Sep 10, 1999 · N839AT · Doug DC932 · Entrance Stairs
  > DURING 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.
- [SDR AT9900657](https://openairdocs.org/sdr/AT9900657.md): Skin · corroded · Sep 9, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR AT9900656](https://openairdocs.org/sdr/AT9900656.md): Skin · corroded · Sep 8, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR AT9900654](https://openairdocs.org/sdr/AT9900654.md): Skin · dented · Sep 8, 1999 · N839AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR AT9900665](https://openairdocs.org/sdr/AT9900665.md): Floor · corroded · Sep 7, 1999 · N839AT · Doug DC932 · Fuselage Floor Panel
  > DURING 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, 51-30
- [SDR AT9900664](https://openairdocs.org/sdr/AT9900664.md): Floor · corroded · Sep 7, 1999 · N839AT · Doug DC932 · Fuselage Floor Panel
  > DURING 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.
- [SDR AT9900662](https://openairdocs.org/sdr/AT9900662.md): Floor · corroded · Sep 7, 1999 · N839AT · Doug DC932 · Fuselage Floor Panel
  > DURING 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.
- [SDR AT9900666](https://openairdocs.org/sdr/AT9900666.md): Cusp · corroded · Sep 5, 1999 · N839AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING 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.

Next page: https://openairdocs.org/deregistered/N839AT-2013-08-16/reports.md?page=2

## 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 = 'N839AT' AND deregistration_id = 'N839AT-2013-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N839AT-2013-08-16/reports

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