# Service difficulty reports: N8969U, cancelled May 6, 2013

A list on [N8969U, cancelled May 6, 2013](https://openairdocs.org/deregistered/N8969U-2013-05-06.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 4 · 184 reports

- [SDR ARWA20041002](https://openairdocs.org/sdr/ARWA20041002.md): Clamp · out of position · Oct 12, 2004 · N8969U · Doug DC862 · Engine Anti-Icing System
  > DURING TAKEOFF ROLL, NR 2 ENGINE EGT REACHED 580 DEGREES CELSIUS, PULLED POWER BACK OIL PRESS LIGHT ILLUMINATED, N1 AND EPR INDICATION ERRATIC. SHUTDOWN ENGINE NR 2; 200 PERCENT N1 5 PERCENT. OIL PRESSURE 10 PSI. FOUND ANTI-ICE DUCT CLAMP OUT OF POSITION, S
- [SDR ARWA20031202](https://openairdocs.org/sdr/ARWA20031202.md): Pitot Head · failed · Dec 6, 2003 · N8969U · Doug DC862 · Pitot/Static System
  > ON CLIMBOUT OF KMIA, CAPTAIN LOST ALTIMETER, AIRSPEED, AND VSI INDICATIONS.
- [SDR ARWA20030803](https://openairdocs.org/sdr/ARWA20030803.md): O-Ring · worn · Aug 13, 2003 · N8969U · Doug DC862 · Aileron Control System
  > LOG PAGE 110832. DISCREPANCY: AT TOP OF DESCEND LOSS OF HYDRAULIC FLUID AND PRESSURE; COMPLETED ABNORMAL HYDRAULIC LANDING CHECKLIST. REMOVED AND REPLACED RT AILERON POWER ACTUATOR HYDRAULIC O-RINGS TO SWIVEL VALVE IAW DC8 MM 27-14-01. PERFORMED LEAK CHECK
- [SDR ARWA20030603](https://openairdocs.org/sdr/ARWA20030603.md): Engine · failed · Jun 11, 2003 · N8969U · Doug DC862 · Engine (Turbine/Turboprop)
  > PRECAUTIONARY SHUTDOWN NR 2 ENGINE; TIME 0030. OIL PRESSURE -0 OIL TEMP 145. ENGINE WINDMILLED 3 1/2 HOURS, ZERO OIL PRESSURE. ALL ABNORMAL PROCEDURES FOLLOWED. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARDS 72-000-30-02-01, 77-000-00-03-1 & 77-000-02-1; A
- [SDR ARWA20030401](https://openairdocs.org/sdr/ARWA20030401.md): Engine · lack of lube · Apr 3, 2003 · N8969U · Doug DC862 · Turbine Engine Oil System
  > AFTER T/O FROM UTP, DURING CLIMB, FE OBSERVER NR 2 OIL QUANITY INDICATOR READING 2 GALLONS & DECREASING. SWAPPED INDICATORS, NO CHANGE. FOLLOWED ABNORMAL PROCEDURES FOR FUEL DUMPING, LANDED (UTP) LESS THAN MLWG. SERVICED NR 2 ENGINE OIL WITH 9 QTS. OF OIL.
- [SDR ARWA20021202](https://openairdocs.org/sdr/ARWA20021202.md): Engine · malfunctioned · Dec 5, 2002 · N8969U · Doug DC862 · Engine (Turbine/Turboprop)
  > PRECAUTIONARY NR 4 ENGINE SHUTDOWN; OIL QUANTITY LOW. TIME: 0605Z, N1: 37 PERCENT. OIL PRESSURE 0-10 PSI. ACCOMPLISHED INFLIGHT ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED NR 4 ENGINE IAW ARROW AIR TASK CARD DC8 UN-003 AND MASTER TALLY UNDER W/O 601627
- [SDR ARWA20021104](https://openairdocs.org/sdr/ARWA20021104.md): Pin · broken · Nov 8, 2002 · N8969U · Doug DC862 · Landing Gear Retraction/Extension System
  > ON GEAR EXTENSION RIGHT HAND MAIN LANDING GEAR DROPPED DOWN WITH A LOUD BANG. FOUND RT MAIN LANDING GEAR CYLINDER RETRACT PIN BROKEN. REMOVED RT MAIN LANDING GEAR. ROUTED TO AAR LANDING GEAR SERVICES FOR REPAIRS. REPAIRED PER DC8 OHM TAPE REVISION 46, DAT
- [SDR ARWA20020905](https://openairdocs.org/sdr/ARWA20020905.md): Hinge · cracked · Aug 28, 2002 · N8969U · Doug DC862 · Fuselage, Door Hinge
  > DURING C-CHECK, MAIN CARGO COMPARTMENT DOOR HINGE LOBE WITH CRACK STA 460.
- [SDR ARWA20020907](https://openairdocs.org/sdr/ARWA20020907.md): Doubler · corroded · Aug 21, 2002 · N8969U · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, COCKPIT STA 133 - STA 148 RBL 63 SUB FLOOR FILLER DOUBLER WITH CORROSION & SHEARED RIVET. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0; REMOVED AND REPLACED RIVET IAW DC-8 SRM 51-1-21.
- [SDR ARWA20020908](https://openairdocs.org/sdr/ARWA20020908.md): Fitting · cracked · Aug 20, 2002 · N8969U · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, MAIN CARGO COMPARTMENT STA 840, L-22R, FITTING WITH CRACK. REMOVED AND REPLACED FITTING OF MAIN CARGO COMPARTMENT IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-1-0.
- [SDR ARWA20020909](https://openairdocs.org/sdr/ARWA20020909.md): Fitting · cracked · Aug 20, 2002 · N8969U · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, MAIN CARGO COMPARTMENT STA 840, L-22L, FITTING WITH CRACK. REMOVED AND REPLACED FITTINGS OF MAIN CARGO COMPARTMENT STA 840, L-22L IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-1-0.
- [SDR ARWA20020910](https://openairdocs.org/sdr/ARWA20020910.md): Support Fitting · cracked · Aug 19, 2002 · N8969U · Doug DC862 · Wing Miscellaneous Structure
  > DURING C-CHECK, RT WING L/E INTERIOR STA XW 239.743 INBOARD PYLON FRONT SPAR SUPPORT FITTING (FOOT STOOL) WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING IAW BOEING MESSAGE INSTRUCTIONS ARW-MIA-02-00020H DATED 08/21/02, S/B DC8-57-84, DC8-A57-84 AND DC8-
- [SDR ARWA20020906](https://openairdocs.org/sdr/ARWA20020906.md): Hinge · cracked · Aug 16, 2002 · N8969U · Doug DC862 · Passenger/Crew Doors
  > DURING C-CHECK, FORWARD ENTRANCE DOOR UPPER HINGE WITH 2 INCH CRACK. REMOVED FORWARD ENTRANCE DOOR IAW DC-8 MM 52-11-1, REMOVED AND REPLACED HINGE AND REINSTALLED FORWARD ENTRANCE DOOR IAW DC-8 MM 52-11-1. OPS CHECK NORMAL IAW DC-8 MM 52-10-0. NO LEAKS NOTE
- [SDR ARWA20020911](https://openairdocs.org/sdr/ARWA20020911.md): Frame · cracked · Aug 16, 2002 · N8969U · Doug DC862 · Fuselage Main, Frame
  > DURING C-CHECK, MAIN CARGO COMPARTMENT 980, L-18R FRAME WITH A 1.75 INCH CRACK. REMOVED AND REPLACED AREA, FABRICATED FILLERS ANGLES AND DOUBLER IAW AS ELEVEN INC DRAWING AS11451 SH 1 & 2, DATED 09/10/02; PRIMED FILLERS, ANGLES & DOUBLER IAW DC-8 SRM 51-1-/ A
- [SDR ARWA20020311](https://openairdocs.org/sdr/ARWA20020311.md): Line · leaking · Mar 24, 2002 · N8969U · Doug DC862 · Engine Pressure Ratio (EPR)
  > DURING CLIMBOUT NR 1 ENGINE FAILED TO PRODUCE APPROPRIATE POWER ALL OTHER ENGINE PARAMETERS NORMAL, PROCEEDED WITH ABNORMAL CHECKLIST AND LANDED WITH NO FURTHER INCIDENTS. PREFORMED EPR CHECK IAW MM 77-11-0, FOUND PT-2 LINE OBSTRUCTED AT INLET GUIDE VANE CAS
- [SDR ARWA20020306](https://openairdocs.org/sdr/ARWA20020306.md): Transformer · malfunctioned · Mar 8, 2002 · N8969U · Doug DC862 · Flight Compartment Lighting
  > SMOKE EMANATED MOMENTARILY FROM RT CORNER OF F/O GLARESHIELD (10 SEC), SMOKE STOPPED AS EMERGENCY CHECKLIST WAS INITIATED. REMOVED AND REPLACED BALLAST TRANSFORMER AND REPLACED LAMPS IAW MM 33-12-0.
- [SDR ARWA0011015](https://openairdocs.org/sdr/ARWA0011015.md): Uplock Switch · dirty · Nov 12, 2001 · N8969U · Doug DC862 · Landing Gear Position and Warning
  > WHILE PERFORMING THE UPLATCH CHECK, LIGHT STAYED ILLUMINATED. COMPLETED ABNORMAL PROCEDURE AND RETURNED TO RODN. LUBRICATED LANDING GEARS AND UPLATCH MECHANISM, CLEANED AND SECURED LT MLG UPLATCH SWITCH IAW MM 32-60-0. OPERATION CHECK NORMAL. AIRCRAFT RETU
- [SDR ARWA0011003](https://openairdocs.org/sdr/ARWA0011003.md): Door · open · Oct 9, 2001 · N8969U · Doug DC862 · Landing Gear Door Retract Section
  > AFTER GEAR RETRACTION LOUD NOISE AND VIBRATION COMING FROM NOSE WHEEL WELL. NOISE DISAPPEARED ON SHORT FINAL WITH GEAR DOWN. OVERWEIGHT LANDING AT PANC. UPON RETURN TO RAMP AFTER SPEAKING TO GROUND CREW FOUND NOSE GEAR DOORS WERE LEFT OPEN. RESET NOSE LAND
- [SDR ARWA0010503](https://openairdocs.org/sdr/ARWA0010503.md): O-Ring · failed · May 25, 2001 · N8969U · Doug DC862 · Hydraulic System, Main
  > ON APPROACH TO TNCC (CURAZAO) LOSS OF HYDRAULIC FLUID. PERFORMED EMERGENCY CHECKLIST AS PER ARROW AIR PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED O-RING FROM NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE ELBOW IAW MM 29-10-12, LEAK CKD OK, OPERA
- [SDR ARWA991003](https://openairdocs.org/sdr/ARWA991003.md): Adc · failed · Oct 28, 1999 · N8969U · Doug DC862 · Air Data Computer
  > MIA - FLT 431 - MODE C INOPERATIVE BOTH TRANSPONDERS. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED OPS CHECK, TESTED AND INSPECTED BOTH ATC TRANSPONDERS. FOUND TO COMPLY WITH FAR 43 APPENDIX 'E' PAR SMALL "C" OPS NORMAL. PERFORMED PITOT STATIC LE
- [SDR 99T64R034](https://openairdocs.org/sdr/99T64R034.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS EXFOLIATED CORROSION AROUND ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED PER EO DRAWING NR 98-047 ON 8110-3 DATED 11/16/98 UNDER WOR 1308. (M)
- [SDR 99T64R033](https://openairdocs.org/sdr/99T64R033.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE SECTION BETWEEN 3 AND 4 PYLONS CORROSION AT FASTENER ATTACH HOLES CENTER OF LEADING EDGE UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-037 ON 8110-3 DATED 11/12/98 UNDER WO 1347. (M)
- [SDR 99T64R032](https://openairdocs.org/sdr/99T64R032.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE 2ND SECTION OUTBOARD NR 4 PYLON CORROSION AT FASTENER ATTACH HOLES UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED PER EO DRAWING NR 98-054 ON 8110-3 DATED 11/23/98 UNDER WO 1347. (M)
- [SDR 99T64R031](https://openairdocs.org/sdr/99T64R031.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > LEFT WING OUTBOARD END AT LEADING EDGE CORROSION ATTACH HOLE AND FOUND CRACK SAME AREA. REMOVED CORROSION PER SRM 51-1-8 AND INSTALLED DOUBLER PER SRM 57-2-1. (M)
- [SDR 99T64R030](https://openairdocs.org/sdr/99T64R030.md): Frame · cracked · Jan 7, 1999 · N8969U · Doug DC862 · Fuselage Main, Frame
  > FOUND A 4.5 INCH CRACK IN FUSELAGE FRAME STATION 759 BETWEEN RL 17 AND 18. STOP DRILL CRACK, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-055 ON 8110-3 DATED 12/03/98 UNDER WO NR 1347. (M)
- [SDR 99T64R029](https://openairdocs.org/sdr/99T64R029.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > LEFT WING FIRST LEADING EDGE SECTION OUTBOARD NR 1 PYLON HAS CORROSION AT FASTENER HOLES MOST INBOARD AFT XFS 578.750. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-035 ON 8110-3 DATED 11/09/98 UNDER WO 1347. (M)
- [SDR 99T64R028](https://openairdocs.org/sdr/99T64R028.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > FOUND CORROSION AT SCREW HOLES NR 4 STUBWING UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-049 ON 8110-3 DATED 11/17/98 UNDER WO 1347. (M)
- [SDR 99T64R027](https://openairdocs.org/sdr/99T64R027.md): Fitting · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Fuselage Miscellaneous Structure
  > W/W RIGHT VERTICAL FITTING FROM LONGERON 24 TO FLOORBEAM AT 879 IS CORRODED. REPLACED FITTING PER 51-1-20 AND EO DRAWING NR 98-032 ON 8110-3 DATED 11/01/98 UNDER WO 1300. (M)
- [SDR 99T64R026](https://openairdocs.org/sdr/99T64R026.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE HAS CORROSION ON BOTTOM SKIN TRAILING EDGE AT WING STATION XFS 341.5. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-038 ON 8110-3 DATED 11/12/98 UNDER WO 1310. (M)
- [SDR 99T64R025](https://openairdocs.org/sdr/99T64R025.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE HAS CORROSION ON BOTTOM SKIN TRAILING EDGE APPROX WING STATION XFS 422.750. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-038 ON 8110-3 DATED 11/12/98 UNDER WO 1310. (M)
- [SDR 99T64R024](https://openairdocs.org/sdr/99T64R024.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > NR 3 STUBWING FORWARD AND INBOARD SLOT WS XS 213 CORROSION REMOVAL BEYOND LIMITS. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-031 ON 8110-3 DATED 10/31/98 UNDER WO 1309. (M)
- [SDR 99T64R023](https://openairdocs.org/sdr/99T64R023.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > NR 3 STUBWING INBOARD TOP TRAILING EDGE STATION XS 220.190 CORROSION BEYOND LIMITS. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-030 ON 8110-3 DATED 10/30/98 UNDER WO 1309. (M)
- [SDR 99T64R022](https://openairdocs.org/sdr/99T64R022.md): Longeron · cracked · Jan 7, 1999 · N8969U · Doug DC862 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT RIGHT LONERON 24 AT STATION 1400 HAS.875 INCH CRACK IN RADIUS. FABRICATED REPAIR CHANNEL AND INSTALLED PER EO DRAWING NR 98-024 ON 8110-3 DATED 10/22/98 UNDER WO 1310. (M)
- [SDR 99T64R021](https://openairdocs.org/sdr/99T64R021.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE CORRODED AT FASTENER HOLE AFT OF INBOARD SLOT DOOR APPROX WS 250. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-029 ON 8110-3 DATED 10/30/98 UNDER WO 1309. (M)
- [SDR 99T64R020](https://openairdocs.org/sdr/99T64R020.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE UPPER SURFACE PANEL HAS.5 INCH CRACK BEHIND NR 3 SLOT AND SMALL BULGE XFS 240.126. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-030 ON 8110-3 DATED 10/30/98 UNDER WO 1310. (M)
- [SDR 99T64R019](https://openairdocs.org/sdr/99T64R019.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE CORROSION AT SCREW OUTBOARD NR 2 PYLON APPROX WS 250 TOP OF WING XFS 335.25. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-039 ON 8110-3, DATED 11/12/98 UNDER WO NR 1310. (M)
- [SDR 99T64R018](https://openairdocs.org/sdr/99T64R018.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > LEFT WING CORROSION AT SEAM OF LEADING EDGE AFT NR 2 PYLON WS 260 TOP OF WING BETWEEN XFS 291.5 AND 304. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-040 ON 8110-3 DATED 11/18/98 UNDER WO 1310. (M)
- [SDR 99T64R017](https://openairdocs.org/sdr/99T64R017.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE PANEL AF TNR 1 PYLON SURFACE CORROSION WS 560 TOP OF WING. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-028 ON 8110-3 DATED 10/30/98 UNDER W/O 1310. (M)
- [SDR 99T64R016](https://openairdocs.org/sdr/99T64R016.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > FOUND LEFT WING LEADING EDGE PANEL OUTBOARD NR 1 PYLON WS 580 TOP OF WING SURFACE CORROSION XFS 641.250. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-035 ON 8110-3 DATED 11/09/98 UNDER WO NR 1309. (M)
- [SDR 99T64R015](https://openairdocs.org/sdr/99T64R015.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > FOUND LEFT WING OUTBOARD LEADING EDGE PANEL RUSTY FASTENERS WS 710-880 TOP OF WING. FOUND CORROSION IN SCREW HOLES, REMOVED CORROSION. FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-027 ON 8110-3 DATED 10/29/98 UNDER WO NR 1309. (M)
- [SDR 99T64R014](https://openairdocs.org/sdr/99T64R014.md): Fitting · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing Miscellaneous Structure
  > RIGHT W/W LONGERON FITTING STATION 920 CORRODED ABOVE LANDING GEAR UPLOCK CYLINDER. REMOVED CORRODED FITTING AND REPLACED WITH NEW FITTING PER SRM 57-3-2 AND SRM 51-1-20 UNDER WO NR 1310. (M)
- [SDR 99T64R013](https://openairdocs.org/sdr/99T64R013.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > SKIN BULGED RIGHT WING CENTER SECTION UPPER SURFACE INBOARD OF OUTBOARD SLOT XFS 520.168. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-037 ON 8110-3 DATED 11/12/98 UNDER WO 1309. (M)
- [SDR 99T64R012](https://openairdocs.org/sdr/99T64R012.md): Nut Plate · missing · Jan 7, 1999 · N8969U · Doug DC862 · Wing Miscellaneous Structure
  > MISSING FASTENERS RIGHT WING LEADING EDGE. OPENED HOLES TO.260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-058 ON 8110-3 DATED 12/13/98 UNDER WO NR 1308. (M)
- [SDR 99T64R011](https://openairdocs.org/sdr/99T64R011.md): Nut Plate · missing · Jan 7, 1999 · N8969U · Doug DC862 · Wing Miscellaneous Structure
  > MISSING FASTENERS LEFT WING LEADING EDGE SECTION. OPEN HOLES TO.260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-057 ON 8110-3 DATED 12/13/98 UNDER WO 1308. (M)
- [SDR 99T64R010](https://openairdocs.org/sdr/99T64R010.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS EXFOLIATED CORROSION AT BOTTOM ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-046 ON 8110-3 DATED 11/17/98 UNDER WO 1308. (M)
- [SDR 99T64R009](https://openairdocs.org/sdr/99T64R009.md): Longeron · damaged · Jan 7, 1999 · N8969U · Doug DC862 · Fuselage Main, Longeron/Stringer
  > FOUND STATION 400-420 STRINGER 19R LOWER FLANGE REMOVED. INSTALLED REPAIR CHANNEL PER EO DRAWING NR 98-056 ON 8110-3 DATED 12/04/98 UNDER WO 1347. (M)
- [SDR 99T64R008](https://openairdocs.org/sdr/99T64R008.md): Angle · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing Miscellaneous Structure
  > CENTER FUEL TANK TOP SIDE AT STATION 857 UNDER NR 4 FLOOR PANEL SURFACE CORROSION AFT TANK ANGLE. REMOVED CORROSION, FLAP PEEN BLENDED AREA PROTECT REWORKED AREA PER EO DRAWING NR 98-025 ON 8110-3 DATED 10/27/98 WO 1308. (M)
- [SDR 99T64R007](https://openairdocs.org/sdr/99T64R007.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS EXFOLIATED CORROSION AT TOP ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-045 ON 8110-3 DATED 11/16/98 WO NR 1308. (M)
- [SDR 99T64R006](https://openairdocs.org/sdr/99T64R006.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZ STABILIZER OUTBOARD LEADING EDGE EXFOLIATED CORROSION TOP ATTACH SCREW HOLES. REMOVED CORROSION FABRICATED DOUBLERS AND INSTALLED PER EO NR 98-044 ON 8110-3 DATED 11/23/98 UNDER WO NR 1308. (M)
- [SDR 99T64R005](https://openairdocs.org/sdr/99T64R005.md): Skin · corroded · Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE FROM XRS 697 TO XRS 885 HAS SCREW HEADS WORKING DUE TO EXFOLIATED CORROSION UPPER SURFACE. REMOVED CORROSION FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-054 ON 8110-3 DATED 11/23/98 UNDER WO NR 1308. (M)

Next page: https://openairdocs.org/deregistered/N8969U-2013-05-06/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 = 'N8969U' AND deregistration_id = 'N8969U-2013-05-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8969U-2013-05-06/reports

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