# Service difficulty reports: N784AL, cancelled Feb 16, 2017

A list on [N784AL, cancelled Feb 16, 2017](https://openairdocs.org/deregistered/N784AL-2017-02-16.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 · 73 reports

- [SDR 22AA20090505](https://openairdocs.org/sdr/22AA20090505.md): Spar · cracked · May 9, 2009 · N784AL · Doug DC863F · Wing Spar
  > ON PRE FLIGHT FOUND FUEL LEAK BY LEFT WING ROOT FORWARD OF WHEEL WELL. UPON FURTHER INVESTIGATION THE LEFT REAR SPAR WAS FOUND CRACKED.
- [SDR 22AA20081203](https://openairdocs.org/sdr/22AA20081203.md): Bleed Valve · stuck · Dec 31, 2008 · N784AL · Doug DC863F · Compressor Bleed Valve
  > LOG PAGE NR 128276. NR 1 ENGINE WOULD NOT ACCELERATE TO TAKE-OFF POWER; REJECTED TAKE OFF AT 80 KTS. - RETURNED TO GATE. FOUND NR 1 COMPRESSOR BLEED VALVE STUCK IN OPEN POSITION. R&R NR 1 ENGINE COMP. BLEED CONTROL VALVE IAW DC-8 M/M 75-30-3; OPS CHECK NOR
- [SDR 22AA20081102](https://openairdocs.org/sdr/22AA20081102.md): Control Cable · broken · Dec 1, 2008 · N784AL · Doug DC863F · Stabilizer Control System
  > ON DESCENT LONG TRIM SUITCASE HANDLE, RIGHT SUITCASE HANDLE JAMMED. FOUND BROKEN CABLE RUNNING NR 49B. REMOVED AND REPLACED 1/16 CONTROL CABLE RUNNING NR 49B IN ACCORDING WITH DC-8 MAINTENANCE MANUAL 27-40-01. RIGGING AND OPERATION CHECKED, FOUND NORMAL IN
- [SDR 22AA20081002](https://openairdocs.org/sdr/22AA20081002.md): Cylinder · malfunctioned · Oct 15, 2008 · N784AL · Doug DC863F · Trailing Edge Flap Actuator
  > ON APPROACH INTO MROC THE FLAPS WOULD NOT EXTEND BEHOND 23 DEGREES. FOUND OUTBOARD FLAP LOCKOUT CYLINDER RETRACTED; SERVICE FLAP LOCKOUT CYLINDERS IAW MM 27-51-10. OPERATIONAL CHECK FOUND NORMAL IAW MM 27-50-00.
- [SDR ARWA20080802](https://openairdocs.org/sdr/ARWA20080802.md): Unknown · sparks · Aug 14, 2008 · N784AL · Doug DC863F · Landing Gear System
  > AIR TURNBACK REPORTED SPARKS COMING FROM RT MAIN GEAR. DECLARED EMERGENCY AND RETURNED TO MIA. (S)
- [SDR ARWA20080201](https://openairdocs.org/sdr/ARWA20080201.md): Limit Switch · malfunctioned · Feb 3, 2008 · N784AL · Doug DC863F · Trailing Flap Position Indicating System
  > DURING TAKEOFF ROLL, TAKEOFF WARNING HORN CAME ON. REMOVED AND REPLACED SI-278 FLAP UPLIMIT SWITCH IN ACCORDANCE WITH M/N 27-52-1 AND SI-177 AND 176 SPOILERS SWITCH IN ACCORDANCE WITH 27-63-1, SYSTEM GROUND TEST NORMAL.
- [SDR ARWA20071205](https://openairdocs.org/sdr/ARWA20071205.md): Snap Ring · loose · Dec 18, 2007 · N784AL · Doug DC863F · Cabin Pressure Control System
  > DURING CLIMB-OUT, UNABLE TO CONTROL THE CABIN PRESSURIZATION, NEITHER WITH AUTO OR MANUAL (WITH 4 T.C. ON). FOUND NR 2 TC DISFUSER SNAP RING LOOSE. REINSTALLED SNAP RING AT NR 2 TC IN ACCORDANCE WITH DC-8 M/M 21-10-6. PRESSURIZATION CHECK FOUND NORMAL IN AC
- [SDR ARWA20061005](https://openairdocs.org/sdr/ARWA20061005.md): Bellcrank · broken · Oct 29, 2006 · N784AL · Doug DC863F · Landing Gear Door Retract Section
  > ON POST FLIGHT FOUND NOSE GEAR DOOR BROKEN LINK. REMOVED TORQUE TUBE AND BELL CRANK IN ACCORDANCE WITH M/M 32-22-2. INSTALLED BELL CRANK AND REINSTALLED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH M/M 32-33-2; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 32-22-1 A
- [SDR ARWA20061004](https://openairdocs.org/sdr/ARWA20061004.md): Wire · damaged · Oct 25, 2006 · N784AL · Doug DC863F · Hydraulic Power System Wiring
  > LOST ALL HYDRAULIC PRESSURE DURING TAXI. REPAIR WIRE ON HYDRAULIC PRESSURE TRANSMITTER IAW MM 20-51-00; OPERATIONAL CHECK NORMAL IAW MM 20-00-00.
- [SDR ARWA20061001](https://openairdocs.org/sdr/ARWA20061001.md): Compressor · stalled · Oct 8, 2006 · N784AL · Doug DC863F · Turbine Engine Compressor Section
  > LOG PAGE NR 124562. ABORTED TAKEOFF AT 105 KTS FOLLOWING NR 4 ENGINE COMPRESSOR STALL. INSPECTED NR 4 ENGINE COMPRESSOR SURGE BLEED VALVE AND TIGHTEN ALL SENCE LINES IAW MM 75-30-01/201; OPERATIONAL CHECK NORMAL ON ENGINE RUN IAW M/M 71-00/501.
- [SDR ARWA20060602](https://openairdocs.org/sdr/ARWA20060602.md): O-Ring · leaking · Jun 28, 2006 · N784AL · Doug DC863F · Hydraulic System, Main
  > PRIOR TO DESCENT, OBSERVED A LOSS OF HYDRAULIC QUANTITY TO THE STAND PIPE LEVEL FOLLOWED BY A LOSS OF PRESSURE. REMOVED AND REPLACED DAMAGE O-RING ON NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE FITTING IN ACCORDANCE WITH M/M 20-12-0 PAGE 211. OPERATIONAL CHECK
- [SDR ARWA20060501](https://openairdocs.org/sdr/ARWA20060501.md): Striker · unknown · May 6, 2006 · N784AL · Doug DC863F · Landing Gear Position and Warning
  > AFTER NORMAL GEAR RETRACTION, RED DOORS NOT LATCHED, LIGHT ILLUMINATED ON UP-LATCH CHECK; PERFORMED ABNORMAL CHECKLIST, LIGHT REMAINED ON. REMOVED AND REPLACED LT MAIN GEAR INBOUND DOOR LATCH STRIKER IN ACCORDANCE WITH M/M 32-31-4; ALSO REPLACED BOTH TARGET A
- [SDR ARWA20060304](https://openairdocs.org/sdr/ARWA20060304.md): Engine · leaking · Mar 29, 2006 · N784AL · Doug DC863F · Turbine Engine Oil System
  > DURING CRUISE, NR 2 ENGINE LOSS OF ALL OIL QUANTITY AND PRESSURE; PRECAUTIONARY ENGINE SHUTDOWN AS PER CHECKLIST (TIME 0655). REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR TASK CARD NR DC8-N-003. LEAK CHECKED, NO LEAKS NOTED; OPERATIONAL CHECK
- [SDR ARWA20060302](https://openairdocs.org/sdr/ARWA20060302.md): Proximity Switch · malfunctioned · Mar 21, 2006 · N784AL · Doug DC863F · Landing Gear Position and Warning
  > "GEAR NOT LATCHED" LIGHT ILLUMINATED AFTER GEAR UPLATCH CHECK; CONTINUED OPERATION AS PER ABNORMAL CHECKLIST. PERFORMED PROXIMITY SWITCHES TEST IN ACCORDANCE WITH M/M 32-60-0. REMOVED AND REPLACED CONTROL BOX PROXIMITY SWITCHES SYSTEM OPERATIONAL CHECK NORMA
- [SDR ARWA20060202](https://openairdocs.org/sdr/ARWA20060202.md): Engine · vibration · Feb 8, 2006 · N784AL · Doug DC863F · Engine (Turbine/Turboprop)
  > SHUT-DOWN NR 3 ENGINE IN FLIGHT DUE TO VIBRATION. COMPLIED WITH ALL CHECKLIST. C/W RED BORDER NR 019421 NR 3 ENGINE P-679000 REPLACEMENT. COMPLY WITH RED BORDER NR 019421; REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH MAINTENANCE MANUAL 71-00-00. OPE
- [SDR ARWA20060218](https://openairdocs.org/sdr/ARWA20060218.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT INTERIOR STA 1620-STA 1640 BETWEEN L-32L & L-33L SKIN WITH CORROSION; N/R 1022- AFT ACCESSORY COMPARTMENT INTERIOR STA 1620 BETWEEN L-30L & L-31L SKIN WITH CORROSION. REPAIR INNER
- [SDR ARWA20060207](https://openairdocs.org/sdr/ARWA20060207.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THRU STA 1720, L-31L THRU L-31R SKIN PANEL WITH CORROSION AT SEVERAL PLACES. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1690 TO FS 1720 AND L-28R TO L-34 IN ACCORDANCE WITH D
- [SDR ARWA20060217](https://openairdocs.org/sdr/ARWA20060217.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Ailerons
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; I/B AILERON BETWEEN XA 565 AND SA 542 LOWER SKIN WITH CORROSION. REMOVED SKIN AND BONDED DOUBLER AND REPLACED BY SOLID SKIN BETWEEN XA 542 AND XW 563 IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-07/05. ISS
- [SDR ARWA20060216](https://openairdocs.org/sdr/ARWA20060216.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Elevator, Plate/Skin
  > DURING "C" CHECK INSPECTION, RT ELEVATOR XE 276 THRU XE 280 LOWER SURFACE WITH CORROSION. REMOVED RT ELEVATOR SKIN UPPER SURFACE XAE 0 TO XE 103 AND XE 273 TO XH 285 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-05-05. ISSUED FAA F
- [SDR ARWA20060215](https://openairdocs.org/sdr/ARWA20060215.md): Skin · delaminated · Feb 3, 2006 · N784AL · Doug DC863F · Elevator, Plate/Skin
  > DURING "C" CHECK INSPECTION, RT ELEVATOR XE 28.843 LOWER SURFACE WITH DELAMINATION. REMOVED RT ELEVATOR SKIN UPPER SURFACE BETWEEN XAE 0 TO SE 103 AND XE 273 TO XE 285 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING AIPSAC-N784AL-05/05. ISSUED FAA FO
- [SDR ARWA20060214](https://openairdocs.org/sdr/ARWA20060214.md): Finger Doubler · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Wing, Center Box
  > DURING "C" CHECK INSPECTION, MAIN CARGO COMPARTMENT STA.920, STA.940, STA.960, XCW 0 - XCW 23 CENTER WING SECCTION RT FINGER DOUBLER WITH CORROSION. REPAIRED FUSELAGE CENTER SECTION PRESSURE PANEL BETWEEN STA 920 AND FS 940 IN ACCORDANCE WITH DRAWING AIPSAC-
- [SDR ARWA20060213](https://openairdocs.org/sdr/ARWA20060213.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, FUSELAGE EXTERIOR BETWEEN STA 1690 & STA 1734 AND L-26L THRU L-28L SKIN WITH CORROSION. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1696 TO FS 1766 AND L-24L TO L-28L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-03/05, SHEETS
- [SDR ARWA20060212](https://openairdocs.org/sdr/ARWA20060212.md): Skin · damaged · Feb 3, 2006 · N784AL · Doug DC863F · Ailerons
  > DURING "C" CHECK INSPECTION, LT O/B AILERON BETWEEN XA 678 AND XA 685 LOWER SKIN RIVETS SHEARED. REMOVED LT O/B AILERON PLATING BETWEEN XA 662 & XA 724 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-09/05, ISSUED FAA FORM 8110-3 APPR
- [SDR ARWA20060210](https://openairdocs.org/sdr/ARWA20060210.md): Structure · cracked · Feb 3, 2006 · N784AL · Doug DC863F · Nacelle/Pylon, Main Frame
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL I/B SIDE WITH 1 - 3/4" CRACK. REMOVED AND REPLACED NR 3 PYLON FOOT STOOL FITTING IN ACCORDANCE WITH DC8 S/B AS7-99 REVISION 1 DATED 09/03/93 AND DC8 S/B AS7-87, REVISION NR 2, DATED 01
- [SDR ARWA20060209](https://openairdocs.org/sdr/ARWA20060209.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 BETWEEN L-30L AND L-31L SKIN WITH CORROSION. REPAIRED INNER DOUBLER BETWEEN FS 1620 AND FS 1680 AND L-26L AND L31L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-06/05, IS
- [SDR ARWA20060206](https://openairdocs.org/sdr/ARWA20060206.md): Skin · corroded · Feb 3, 2006 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STATION 1490 THROUGH STATION 1690L, L-31L THRU L31R SKIN PANEL WITH CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED SKIN FROM FUSELAGE STA 1490 TO FS STA 1690 IN ACCORDANCE WITH AIPSAR EA
- [SDR ARWA20050908](https://openairdocs.org/sdr/ARWA20050908.md): Skin · corroded · Jul 18, 2005 · N784AL · Doug DC863F · Ailerons
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT INBOUND AILERON BETWEEN XA 565 AND XA542 LOWER SKIN WITH CORROSION.
- [SDR ARWA20050906](https://openairdocs.org/sdr/ARWA20050906.md): Skin · corroded · Jul 14, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1690 THROUGH STA 1734, L-29L, SKIN WITH CORROSION.
- [SDR ARWA20050907](https://openairdocs.org/sdr/ARWA20050907.md): Structure · cracked · Jul 12, 2005 · N784AL · Doug DC863F · Nacelle/Pylon Miscellaneous Structure
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 2 PYLON FOOT STOOL INBOUND SIDE WITH CRACK, APPROXIMATELY 5/8".
- [SDR ARWA20050905](https://openairdocs.org/sdr/ARWA20050905.md): Structure · cracked · Jul 12, 2005 · N784AL · Doug DC863F · Nacelle/Pylon Miscellaneous Structure
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL INBOUND SIDE WITH 1.750 INCH CRACK.
- [SDR ARWA20050904](https://openairdocs.org/sdr/ARWA20050904.md): Skin · corroded · Jul 7, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 THROUGH STA 1640, BETWEEN L-32L AND L-33L, SKIN WITH CORROSION.
- [SDR ARWA20050903](https://openairdocs.org/sdr/ARWA20050903.md): Skin · corroded · Jun 23, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THROUGH STA 1720, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES.
- [SDR ARWA20050902](https://openairdocs.org/sdr/ARWA20050902.md): Skin · corroded · Jun 23, 2005 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1490 THROUGH STA 1690, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES.
- [SDR ARWA20050505](https://openairdocs.org/sdr/ARWA20050505.md): Connector · dirty · May 11, 2005 · N784AL · Doug DC863F · Fire Detection
  > DURING MAINTENANCE INSPECTION, NR 2 FIRE WARNING DOES NOT TEST; NO LIGHT; NO BELL. CLEANED NR 2 FIRE CONNECTOR WARNING; OPERATIONAL CHECK TEST NORMAL IN ACCORDANCE WITH M/M 26-10-0.
- [SDR ARWA20050108](https://openairdocs.org/sdr/ARWA20050108.md): Landing Gear · lack of lube · Jan 30, 2005 · N784AL · Doug DC863F · Main Landing Gear
  > GEAR NOT LATCHED LIGHT ILLUMINATED. REMAINED ILLUMINATED AFTER COMPLETING GEAR NOT LATCHED LIGHT ILLUMINATED CHECKLIST. CHECK LANDING GEAR MECHANISM, LUBRICATED SAME, PERFORM GEAR SWING IN ACCORDANCE WITH MM 32-30-0. ALL LIGHTS OPERATED OK IN ACCORDANCE WIT
- [SDR ARWA20050106](https://openairdocs.org/sdr/ARWA20050106.md): Engine · malfunctioned · Jan 25, 2005 · N784AL · Doug DC863F · Engine (Turbine/Turboprop)
  > NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED; OIL PRESS GAUGE INDICATED 25 PSI, FOLLOWED BY A LOSS OF OIL QUANTITY, WENT TO ZERO. PERFORMED OIL PRESSURE LIGHT ILLUMINATED CHECKLIST; THEN, PERFORMED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL CHECKLIST. ENGINE SHUTDOWN
- [SDR ARWA20050102](https://openairdocs.org/sdr/ARWA20050102.md): Warning Light · illuminated · Jan 12, 2005 · N784AL · Doug DC863F · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, GEAR NOT LATCHED LIGHT REMAINTED ILLUMINATED, PERFORMED ABNORMAL CHECKLIST. CHECKED ALL WIRING FOR GEAR LATCH LIGHT. JACKED A/C PERFORMED GEAR SWING SEVERAL TIMES. CHECK ALL THREE GEARS FOR CONDITION AND FOUND NORMAL. UNABLE TO DUPLI
- [SDR ARWA20041008](https://openairdocs.org/sdr/ARWA20041008.md): Indicator · inoperative · Oct 27, 2004 · N784AL · Doug DC863F · Weather Radar System
  > LOST WEATHER RADAR IN ROUTE TO GEG. REMOVED AND REPLACED RADAR INDICATOR AND RADAR R/T, OPERATIONS TESTED NORMAL IN ACCORDANCE WITH M/M 34-41-1.
- [SDR ARWA20040806](https://openairdocs.org/sdr/ARWA20040806.md): Link Assy · failed · Aug 30, 2004 · N784AL · Doug DC863F · Landing Gear Door Retract Section
  > AFTER TAKEOFF, HAD A VIBRATION BELOW COCKPIT AREA RECYCLED LANDING; GEAR NO HELP; RETURNED TO DEPARTURE (KMIA. REMOVED AND REPLACED RT NOSE GEAR DOOR LINK ASSEMBLY IAW MM 32-22-2. OPERATIONAL CHECK NORMAL.
- [SDR ARWA20040501](https://openairdocs.org/sdr/ARWA20040501.md): Indicator · malfunctioned · May 5, 2004 · N784AL · Doug DC863F · Altimeter, Barometric/Encoder
  > STANDBY ALTITUDE INDICATOR FAILED IN FLIGHT. REMOVED STANDBY INDICATOR & REPLACED WITH SERVICE STANDBY ATT. INDICATOR. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DACO DC-8 MM 24-3-3.
- [SDR ARWA20040502](https://openairdocs.org/sdr/ARWA20040502.md): Wire · damaged · May 5, 2004 · N784AL · Doug DC863F · Engine Oil System Wiring
  > NR 1 OIL TEMPERATURE ERRATIC AND UNREALIABLE IN-FLIGHT. REPAIRED WIRE AT PIN U NR 1 ENGINE PYLON MAIN DISCONNECT PLUG IN ACCORDANCE WITH DACO DC-8 MM 20-50-1. RAN ENGINE FOR 20 MINUTES. OPERATIONAL CHECK GOOD IAW DACO DC-8 MM 71-00-00
- [SDR ARWA20031105](https://openairdocs.org/sdr/ARWA20031105.md): Compressor · stalled · Nov 30, 2003 · N784AL · Doug DC863F · Turbine Engine Compressor Section
  > ON FLIGHT 410, THE NR 4 ENGINE COMPRESSOR STALLED, FOLLOWED BY LOSS OF POWER. ACCOMPLISHED IN FLIGHT ENGINE SHUTDOWN AS PER FOM; ENGINE SHUTDOWN AT 14:35, THE WINDMILLING OIL PRESSURE WAS ZERO.
- [SDR ARWA20031101](https://openairdocs.org/sdr/ARWA20031101.md): Brake Assy · damaged · Nov 9, 2003 · N784AL · Doug DC863F · Brake
  > AIRCRAFT DOES NOT TAXI UNDER IT'S OWN POWER. FOUND NR 6 BRAKE ASSEMBLY DAMAGED. REMOVED AND REPLACED BRAKE ASSEMBLY IAW DC8 MM 32-42-1 AND MAIN WHEEL ASSEMBLY IAW MM 32-40-1. OPERATIONAL CHECK NORMAL.
- [SDR ARWA20031001](https://openairdocs.org/sdr/ARWA20031001.md): Link · broken · Oct 14, 2003 · N784AL · Doug DC863F · Trailing Edge Flap Control System
  > ON APPROACH, WHEN SELECTING FLAPS 23 DEGREES AIRCRAFT ROLLED TO THE LEFT WITH SPLIT FLAP INDICATION, ON POST FLIGHT FOUND RT INBOARD FLAP BRACKET BROKEN. RECORD FOR 27-268. REMOVED AND REPLACED RT INBOARD FLAP IAW MM 27-51-4. OPERATIONAL CHECK NORMAL IAW 27
- [SDR ARWA20030705](https://openairdocs.org/sdr/ARWA20030705.md): Spring · broken · Jul 10, 2003 · N784AL · Doug DC863F · Landing Gear Door Retract Section
  > LOG PAGE 102010. AFTER TAKEOFF, DOORS NOT LATCHED LIGHT ILLUMINATED. FOUND BROKEN SPRING AT RT MAIN LANDING GEAR DOOR CONTROL VALVE MECHANISM. REPLACED SPRING IAW MM 32-32-7, PERFORMED GEAR SWING IAW MM 32-30-0; FOUND NORMAL SYSTEM.
- [SDR ARWA20030512](https://openairdocs.org/sdr/ARWA20030512.md): Skin · corroded · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR SURFACE WITH CORROSION, STATION 510, L-35R. REPAIRED FUSELAGE LOWER SKIN AT FUSELAGE STA 510 AND L-35R IAW AVITAS ENGINEERING REPAIR ORDER AROW-031RO-5, PAGE 1 & 2, DATED 05/01/03 AND REPAIR
- [SDR ARWA20030511](https://openairdocs.org/sdr/ARWA20030511.md): Skin · corroded · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT FUSELAGE INNER SKIN WITH CORROSION BETWEEN STATION 1660 AND STATION 1680, BETWEEN L-24R AND L-25R. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED AREA
- [SDR ARWA20030510](https://openairdocs.org/sdr/ARWA20030510.md): Skin · corroded · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR LOWER SURFACE RIVET PLUNGED, STATION 540, BY L-36. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, TRIMMED
- [SDR ARWA20030509](https://openairdocs.org/sdr/ARWA20030509.md): Doubler · corroded · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT STATION 1620, BETWEEN L-26R AND L-31R INNER SKIN WITH SEVERAL SPOTS OF CORROSION. REPAIRED FUSELAGE INNER DOUBLER AT FS 1620, BETWEEN L-25R AND L-31R IAW MFG ENGINEERING REPAIR O
- [SDR ARWA20030508](https://openairdocs.org/sdr/ARWA20030508.md): Fitting · cracked · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Longeron/Stringer
  > N/R 421. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 879, L-24R FITTING WITH CORROSION AND 3 INCH CRACK. REMOVED AND REPLACED FITTING OF R/H MAIN LANDING GEAR WHEEL WELL STA 879, L-24R IAW SRM 51-1-20D AND SR

Next page: https://openairdocs.org/deregistered/N784AL-2017-02-16/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 = 'N784AL' AND deregistration_id = 'N784AL-2017-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N784AL-2017-02-16/reports

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