# Service difficulty reports: N1804, cancelled Nov 8, 2013

A list on [N1804, cancelled Nov 8, 2013](https://openairdocs.org/deregistered/N1804-2013-11-08.md).

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

- [SDR ARWA20021201](https://openairdocs.org/sdr/ARWA20021201.md): Windshield · Dec 1, 2002 · N1804 · Doug DC862 · Flight Compartment Windows
  > LOG PAGE # 109140. DISCREPANCY: APPROACHING FL350, CAPTAIN'S WINDSHIELD DEVELOPED MULTIPLE CRACKS. CORRECTIVE ACTION: REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-2; ALSO CAPTAIN'S WINDSHIELD CONTROLLER IAW MM 30-41-1. FOUND NORMAL OPS CHECK.
- [SDR ARWA20020903](https://openairdocs.org/sdr/ARWA20020903.md): Transceiver · failed · Sep 7, 2002 · N1804 · Doug DC862 · Weather Radar System
  > NR 2 RADAR ON CAPTAIN'S SIDE WILL NOT PAINT GROUND RETURNS OR WEATHER. NR 2 RADAR ON FIRST OFFICER'S SIDE WILL NOT PAINT GROUND RETURN OR WEATHER AND RADAR SPIKES. AIRCRAFT RETURNED TO DEPARTING BASE. REMOVED AND REPLACED NR 2 RADAR TRANSCEIVER IAW MM 34-0
- [SDR ARWA20020902](https://openairdocs.org/sdr/ARWA20020902.md): Bleed Valve · Sep 3, 2002 · N1804 · Doug DC862 · Compressor Bleed Valve
  > LOG PAGE # 112879. DISCREPANCY: DURING TAXI NOTICED # 3 ENGINE COMPRESSOR STALLING ACCELERATION OF ENGINE. CORRECTIVE ACTION: REMOVED AND REPLACED # 3 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3. OPERATIONS CHECKED OK; RUNUP FOUND NORMAL IAW DC-8 MM 71-00
- [SDR ARWA20020507](https://openairdocs.org/sdr/ARWA20020507.md): Spar · cracked · May 7, 2002 · N1804 · Doug DC862 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING C-CHECK, NR 4 PYLON INTERIOR, STA YN 165, RM UPPER CHORD WITH 4 INCH CRACK. REPAIRED UPPER SPAR CAP OF NR 4 PYLON IAW AS ELEVEN INC DRAWING AS 11403, SHEET 1 TO 6. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.
- [SDR ARWA20020502](https://openairdocs.org/sdr/ARWA20020502.md): Splice · cracked · May 6, 2002 · N1804 · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FORWARD LOWER CARGO COMPARTMENT FUSELAGE FS 340, FS 360, FS 380, FS 400, FS 420, FS 440 & FS 460; LBL 62.5 FLOORBEAM SPLICE WITH 2.750 INCH CRACK. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE IAW AS ELEVEN INC DRAWING AS 11077, SHEET 1 OF 9, DA
- [SDR ARWA20020501](https://openairdocs.org/sdr/ARWA20020501.md): Longeron · cracked · May 6, 2002 · N1804 · Doug DC862 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON L-21L AT FUSELAGE FS 280 WITH 2 INCH CRACK. FABRICATED SHIM & REPAIR ANGLE IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. INSTALLED PARTS IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. ISSUED FAA FORM
- [SDR ARWA20011211](https://openairdocs.org/sdr/ARWA20011211.md): Fitting · excess play · Dec 20, 2001 · N1804 · Doug DC862 · Landing Gear Position and Warning
  > DEPARTING KATL, GEAR NOT LATCHED LIGHT ILLUMINATED. ABNORMAL CHECKLIST COMPLETED AND LIGHT DID NOT EXTINGUISH, AFTER EACH UPLATCH CHECK (IN UPLATCH CHECK POSITION). CORRECTED PLAY AT RIGHT MLG UPLOCK ROLLER FITTING, ALSO LUBRICATED ALL GEARS. LANDING GEAR O
- [SDR ARWA20011205](https://openairdocs.org/sdr/ARWA20011205.md): Engine · Dec 11, 2001 · N1804 · Doug DC862 · Engine Fuel and Control
  > LOG PAGE 101856. DISCREPANCY: ON ADVANCING THROTTLE FOR TAKE OFF #4 ENGINE HUNG, CARRIED OUT ABNORMAL PROCEDURE FOR ENGINE HUNG WITH THRUST LEVER IN REVERSE ENGINE STARTED TO ACCELERATE. CANCELED REVERSE THRUST ENGINE CONTINUED TO ACCELERATE WITH THROTTLE CLOS
- [SDR ARWA0011008](https://openairdocs.org/sdr/ARWA0011008.md): Indicator · inoperative · Oct 16, 2001 · N1804 · Doug DC862 · Directional Gyro and Indicating System
  > CAPTAIN COMPASS INOP, RETURNED TO KMIA. REMOVED AND REPLACED PICTORIAL DEVIATION INDICATOR IAW MM 34-00. PERFORMED OPERATIONAL CHECK IAW 34-21-0, FOUND ALL SYSTEMS NORMAL.
- [SDR ARWA0010602](https://openairdocs.org/sdr/ARWA0010602.md): Selector Valve · leaking · Jun 3, 2001 · N1804 · Doug DC862 · Hydraulic System, Main
  > HYDRAULIC PRESS LOST OUT OF SLLP. AILERON AND RUDDER POWER LIGHTS CAME ON, CHECKLISTS WERE COMPLETED AND DIVERTED TO SPIM. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HYDRAULIC SYSTEM SELECTOR VALVE IAW MM 29-10-18. OPERATIONAL CHECKED OK, NO LE
- [SDR ARWA000401](https://openairdocs.org/sdr/ARWA000401.md): Engine · malfunctioned · Apr 6, 2000 · N1804 · Doug DC862 · Turbine Engine Oil System
  > MIA - FLT 517 - NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY DROPPED TO.5 GALLON. A PRECAUTIONARY ENGINE SHUTDOWN WAS PERFORMED. OIL PRESSURE WAS DECREASING AND OIL TEMP WAS INCREASING. MAX TEMP WAS 125 CELSIUS AND LOWEST OIL PRESSURE WAS 37
- [SDR ARWA990703](https://openairdocs.org/sdr/ARWA990703.md): Outflow Valve · lack of lube · Jul 25, 1999 · N1804 · Doug DC862 · Pressure Regulator/Outflow Valve
  > MIA - FLT 627 - UNABLE TO PRESSURIZE AIRCRAFT IN AUTO OR MANUAL DURING TAKEOFF. DUMPED FUEL AND RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT INVESTIGATED FOR DEFECTS. PRESSURIZATION NORMAL IAW MM 21-30-00. LUBED OUTFLOW VALVE AS PRECAUTIONARY. CHECKED NORMA
- [SDR ARWA990701](https://openairdocs.org/sdr/ARWA990701.md): Wheel · failed · Jun 27, 1999 · N1804 · Doug DC862 · Wheel/Ski/Float
  > CLO - FLT 627 - INBOURND TO CALI, MESSAGE THAT MLG TIRE HAD SEPARATED FROM AIRCRAFT ON TAKEOFF FROM QUITO, ECUADOR. AIRCRAFT LANDED IN CALI WITHOUT INCIDENT. INSPECTION FOUND NR 2 MLG OUTBOARD WHEEL HALF BEAD HAD SEPARATED AND TIRE EJECTED. INCURRED DAMAGE
- [SDR ARWA990307](https://openairdocs.org/sdr/ARWA990307.md): Oil Pump · failed · Mar 25, 1999 · N1804 · Doug DC862 · Turbine Engine Oil System
  > MIA - NR 4 ENGINE OIL PRESSURE DROPPED TO 32 PSI. SHUTDOWN ENGINE AS PER ABNORMAL CHECKLIST. WINDMILL SPEEDS WERE N1, 13.5 PERCENT, N2 21 PERCENT, OIL PRESS 3 PSI. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE OIL PUMP ASSY
- [SDR ARWA981221](https://openairdocs.org/sdr/ARWA981221.md): Fcu · failed · Dec 29, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine Engines
  > PNX - FLT 515 - BLOCK TURNBACK, ON RIGHT RUNUP, NR 1 ENGINE DIDN'T ACCELERATE. ALL INDICATIONS REMAINED IN IDLE. INDICATION WITH SLIGHTLY FLUCTUATING EPR NEEDLE. FELT ENGINE VIBRATING AND HEARD 'KNOCKING' NOISE. IMMEDIATELY BROUGHT THROTTLE BACK TO IDLE A
- [SDR IH987518001](https://openairdocs.org/sdr/IH987518001.md): Strut · damaged · Dec 7, 1998 · N1804 · Doug DC862 · Main Landing Gear Strut/Axle/Truck
  > UPON DISASSEMBLY OF RT MLG STRUT FOR SEAL CHANGE, P/N 3598295 FOLLOWER FOUND TO BE FRACTURED CAUSING DAMAGE TO P/N 37673709-501 ADAPTER ASSY PACKING, P/N 3598375 SPACER. UPPER BEARING SPLIT, P/N 3598297 HEAD, PISTON, AND P/N 3598296 VALVE, REBOUND CHECK. VIS
- [SDR ARWA981064](https://openairdocs.org/sdr/ARWA981064.md): Vert Gyro · malfunctioned · Oct 30, 1998 · N1804 · Doug DC862 · Attitude Gyro and Indicating System
  > CAPT'S ADI GYRO FAILS IN ALL TURNS INTERMITTENTLY IN LEVEL FLIGHT ALSO WINDSHEAR FAIL ILUMINATED AT THE SAME TIME. R/R #1 VERT. GYRO I.A.W. DC-8 M/M 34-25-1 OPS CHECK OF HORIZONTAL SYSTEM, GOOD ON GROUND I.A.W. DC-8 M/M 34-25-0.
- [SDR ARWA980602](https://openairdocs.org/sdr/ARWA980602.md): Fuel Contl Unit · failed · Jun 6, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine Engines
  > AIR TURNBACK, AFTER DEPARTURE NR 3 ENGINE UNSPOOLED AND WHEN POWER LEVER WAS ADVANCED ENGINE WOULD NOT ACCELERATE. RETURNED TO TUS WITHOUT INCIDENT. INSPECTED ENGINE INLET, TAILPIPE, OIL AND FUEL FILTERS. NO DEFECTS NOTED. REMOVED AND REPLACED FCU, MAIN OI
- [SDR ARWA980506](https://openairdocs.org/sdr/ARWA980506.md): Mechanism · out of adjust · May 19, 1998 · N1804 · Doug DC862 · Landing Gear Door Retract Section
  > IN FLT RETURN DUE TO LOUD RATTLING NOISE FROM NOSE WHEEL WELL AREA. UNABLE TO PRESSURIZE AIRCRAFT AUTO OR MANUALLY. ADJUSTED NOSE GEAR DOOR PER MM 32-10-0. RUN UP ENGINES PRESSURIZED OK IN MANUAL, AUTO INOP OPEN DMI ON AUTO PRESS. (M)
- [SDR ARWA980407](https://openairdocs.org/sdr/ARWA980407.md): Hyd Line · leaking · Apr 20, 1998 · N1804 · Doug DC862 · Hydraulic System, Main
  > LOST HYDRAULIC FLUID TO STAND PIPE LEVEL, HYDRAULIC LOSS OF FLUID, EMERGENCY CHECKLIST WAS PERFORMED. PRESSURE CHECK OK. ABNORMAL CHECKLIST WAS FOLLOWED TO AND BEFORE LANDING CHECKS. LANDING AND ROLL-OUT WERE UNEVENTFUL. PRECAUTIONARY A/C TOW IN WAS REQUES
- [SDR ARWA980309](https://openairdocs.org/sdr/ARWA980309.md): Link · bent · Mar 30, 1998 · N1804 · Doug DC862 · Cargo/Baggage Doors
  > ON OPENING OF MAIN CARGO DOOR FOUND FOUR LONG LINK ASSYS BENDING. REMOVED AND REPLACED 4 LONG LINK ASSY FOR FWD ACTUATOR END, FOUR ACT. AFT AND FWD IAW CARGO CONVERSION MM CHIP 7-08. OPS NORMAL ALL INDICATIONS NORMAL SEVERAL TIMES.
- [SDR ARWA980207](https://openairdocs.org/sdr/ARWA980207.md): Bolt · sheared · Feb 24, 1998 · N1804 · Doug DC862 · Aileron Control System
  > UNABLE TO MOVE AILERONS IN MANUAL TO RIGHT. UNABLE TO MOVE RIGHT RUDDER PEDAL UPON FURTHER INSPECTION FOUND SHEARED BOLT AT LT MANUAL REVERSION MECHANISM LINKAGE JAMMING LINKAGE. REMOVED AND REPLACED BOLT, AILERON REVERSION SYSTEM OPS. CHECKED NORMAL IN MAN
- [SDR ARWA980201](https://openairdocs.org/sdr/ARWA980201.md): Engine · failed · Feb 2, 1998 · N1804 · Doug DC862 · Engine (Turbine/Turboprop)
  > CHECK NR 2 ENGINE FOR VIBRATIONS NR 2 THROTTLE AND START LEVEL HARD IN CRUISE. ACCOMPLISHED R/B 8269 REMOVED AND REPLACED NR 2 ENGINE IAW ARROW AIR J/C 6519 AND J/C 6528, OPERATIONS AND LEAK CHECKED NORMAL ON RUN UP, IAW J/C 6527.
- [SDR ARWA971006](https://openairdocs.org/sdr/ARWA971006.md): Filter · defective · Oct 29, 1997 · N1804 · Doug DC862 · Turbine Engine Oil System
  > NR 2 ENGINE OIL PRESSURE ILLUMINATED, PERFORMED ABNORMAL CHECKLIST, LIGHT GOES OUT AFTER THROTTLE RETRACTED PARAMETERS MONITORED CONTINUED NORMAL OPERATION. DURING APPROACH LIGHT CAME ON, ENGINE PRECAUTIONARY SHUT DOWN AT 05044 Z. REMOVED AND REPLACED MAIN O
- [SDR ARWA970604](https://openairdocs.org/sdr/ARWA970604.md): Cap · missing · Jun 19, 1997 · N1804 · Doug DC862 · Hydraulic Reservoir, Main
  > HYDRAULIC FAILURE IN CRUISE, HYD PRESS ZERO WITH MAIN PUMPS OR AUX PUMP, QUANTITY AND TEMP OK. FOUND MAIN HYD RESERVOIR CAP MISSING. REFILLED 15 GAL OF HYD FLUID. PERFORMED COMPLETE HYD POWER SYSTEM IAW MM 29-00. INSTALLED AND SAFETIED NEW CAP.
- [SDR ARWA970601](https://openairdocs.org/sdr/ARWA970601.md): Battery Pack · discharged · Jun 17, 1997 · N1804 · Doug DC862 · Emergency Lighting
  > MIA - FLT 615 - DURING PRE-FLIGHT INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECK NORMAL IAW MM 33-50-1. AMENDMENT TO ORIGINAL ARWA970601. (X)
- [SDR 95ZZZX6354](https://openairdocs.org/sdr/95ZZZX6354.md): Antenna · malfunctioned · Oct 27, 1995 · N1804 · Doug DC862 · Weather Radar System
  > AIR TURN-BACK, RADAR UNRELIABLE AND PAINTING ERRATICALLY. REPLACED RADAR ANTENNA; OPS CHECK NORMAL.
- [SDR 95ZZZM668](https://openairdocs.org/sdr/95ZZZM668.md): Skin · corroded · Oct 16, 1995 · N1804 · Doug DC862 · Wing, Plate/Skin
  > DURING B-3 INSPECTION, FOUND LEVEL 2 CORROSION AT LEFT WING LEADING EDGE ATTACH POINT STATION X 526. CORROSION REMOVED AND FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER OF.63 INCH 7075T6 AND.071 INCH 7075T6. PRIMED WITH ALODINE
- [SDR 95ZZZM667](https://openairdocs.org/sdr/95ZZZM667.md): Relief Valve · stuck open · Oct 9, 1995 · N1804 · Doug DC862 · Turbine Engine Oil System
  > AFTER 27 MINUTES FLIGHT TIME, NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN AT 13:45Z. UPON INSPECTION AT BRO, FOUND OIL PRESSURE RELIEF VALVE NOT REGULATING. REPLACED RELIEF VALVE. ENGINE OPS CHECK NORMAL IAW MM 79-32-0.
- [SDR AR091351](https://openairdocs.org/sdr/AR091351.md): Skin · cracked · Sep 13, 1995 · N1804 · Doug DC862 · Fuselage Main, Plate/Skin
  > FUSELAGE OUTER SKIN CRACKED 1.50 INCHES IN UPPER AFT CORNER OF FWD ENTRY DOOR CUT-OUT. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC-8 SB 53-075, AND DAC DWG SR 0850021. BLIND FASTENERS TO BE REPLACED AT NEXT C-CHECK PER DACO FAX DATED 9-15-95. (X)
- [SDR 95ZZZX3452](https://openairdocs.org/sdr/95ZZZX3452.md): Skin · corrosion · Jul 6, 1995 · N1804 · Doug DC862 · Leading Edge Devices
  > LEFT WING INBOARD SLOT L/E HAS LEVEL 2 CORROSION. REPAIRED IAW SRM 57-2-1.
- [SDR 95ZZZX3453](https://openairdocs.org/sdr/95ZZZX3453.md): Fitting · cracked · Jul 5, 1995 · N1804 · Doug DC862 · Elevator Structure
  > DURING PRE-FLIGHT, MAINTENANCE CHECK FOUND LT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0.
- [SDR 95ZZZM266](https://openairdocs.org/sdr/95ZZZM266.md): Fitting · cracked · Jul 5, 1995 · N1804 · Doug DC862 · Elevator Structure
  > DURING PREFLIGHT MAINTENANCE CHECK, FOUND LEFT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0.
- [SDR 95ZZZX3457](https://openairdocs.org/sdr/95ZZZX3457.md): Floor Support · cracked · Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING B-CHECK INSPECTION, FOUND RIGHT WW AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACKED AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39.
- [SDR 95ZZZX3451](https://openairdocs.org/sdr/95ZZZX3451.md): Angle · cracked · Jul 3, 1995 · N1804 · Doug DC862 · Trailing Edge Flaps
  > DURING B-CHECK INSPECTION, THE RT INBOARD FLAP, OUTBOARD, FORMER AND SCISSOR PANEL ATTACHMENT ANGLES FOUND CRACKED IN 2 LOCATIONS, BOTTOM AREA. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE IAW DER ARW 12565-128.
- [SDR 95ZZZX3449](https://openairdocs.org/sdr/95ZZZX3449.md): Floor Support · cracked · Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE RT W/W AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACK AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39.
- [SDR 95ZZZM268](https://openairdocs.org/sdr/95ZZZM268.md): Longeron · corroded · Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Main, Longeron/Stringer
  > POPPED RIVET HEADS AND SKIN BULGE AT FS 208.00 AT LONGERON 28R. REMOVED SECTION OF LONGERON 28R AND TWO INTERCOSTALS. FOUND LEVEL 2 CORROSION ON L-28R. REPLACED 20 INCH SECTION OF L-28R AND REINSTALLED INTERCOSTALS PICKING EXISTING HOLES IAW SRM 53-2-2 AND 5
- [SDR 95ZZZM265](https://openairdocs.org/sdr/95ZZZM265.md): Skin · corroded · Jul 3, 1995 · N1804 · Doug DC862 · Elevator, Plate/Skin
  > LEFT ELEVATOR LOWER SKIN HAS LEVEL 2 CORROSION AT XE 195.33. SKIN SECTION REMOVED. FABRICATED NEW SKIN USING OLD AS TEMPLATE. INSTALLED NEW SKIN SECTION IAW SRM 55-2-0, 51-1-8 AND 51-1-21. REBALANCED ELEVATOR IAW SRM 51-4-4, DC8 SB 27-185 AND DOUGLAS FAX F
- [SDR 95ZZZM267](https://openairdocs.org/sdr/95ZZZM267.md): Te Skin · corroded · May 29, 1995 · N1804 · Doug DC862 · Elevator, Plate/Skin
  > FOUND LEVEL 2 CORROSION LEFT ELEVATOR OUTBOARD STATIC WICK ATTACH POINT. REMOVED LEFT ELEVATOR. REMOVED DAMAGED T/E SECTION. FABRICATED AND INSTALLED NEW T/E SECTION IAW SRM 51-1-21A. INSTALLED NEW STATIC WICK BASE IAW MM 23-60-00. REINSTALLED ELEVATOR AF
- [SDR 95ZZZX3450](https://openairdocs.org/sdr/95ZZZX3450.md): Slot Door · corrosion · Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/Skin
  > ON A TYPE SERVICE 'A', FOUND RT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS' HEADS. CUT OUT DAMAGED AREAS, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED IAW SRM 57-2-1, FIGURE 2H.
- [SDR 95ZZZW658](https://openairdocs.org/sdr/95ZZZW658.md): Slot Door · corroded · Apr 25, 1995 · N1804 · Doug DC862 · Leading Edge Devices
  > ON 'A' CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL II CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE.
- [SDR 95ZZZW657](https://openairdocs.org/sdr/95ZZZW657.md): Slot Door · corroded · Apr 25, 1995 · N1804 · Doug DC862 · Leading Edge Devices
  > ON 'A' CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL II CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. (W)
- [SDR 95ZZZM264](https://openairdocs.org/sdr/95ZZZM264.md): Slot Door · corroded · Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/Skin
  > ON A-CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE. REMOVED SLOT DOOR L/E SECTION, CUT OUT DAMAGED AREAS, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/E.
- [SDR 95ZZZM263](https://openairdocs.org/sdr/95ZZZM263.md): Slot Door · corroded · Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/Skin
  > ON A-CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. REMOVED SLOT DOOR L/E. CUT OUT DAMAGED AREAS, FABRICATED ADN INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/E

## 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 = 'N1804' AND deregistration_id = 'N1804-2013-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N1804-2013-11-08/reports

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