# Service difficulty reports: N1808E, cancelled Mar 10, 2017

A list on [N1808E, cancelled Mar 10, 2017](https://openairdocs.org/deregistered/N1808E-2017-03-10.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 · 161 reports

- [SDR ARWA20020207](https://openairdocs.org/sdr/ARWA20020207.md): Compressor · stalled · Feb 26, 2002 · N1808E · Doug DC862 · Turbine Engine Compressor Section
  > UPON COMMENCING T/O ROLL NR 2 ENGINE COMPRESSOR STALLED SPEED NIL WIND CALM. AIRCRAFT RETURNED TO THE RAMP. PERFORMED VISUAL INSPECTION OF NR 2 ENGINE IN ACCORDANCE WITH 71-00, OPS CHECKED FOUND NORMAL ON GROUND RUN UP.
- [SDR ARWA20020105](https://openairdocs.org/sdr/ARWA20020105.md): Valve · Jan 5, 2002 · N1808E · Doug DC862 · Compressor Bleed Valve
  > LOG PAGE 108167. DISCREPANCY:ON ATART UP WHEN # 2 ENGINE THROTTLE IS ADVANCED ENGINE SURGES AND VIBRATES. WHEN REVERSE IS SELECTED TR TRANSLATES AND BUCKET DEPLOYS BUT ENGINE DOES NOT ACCELERATE IN REVERSE. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE SUR
- [SDR ARWA20011116](https://openairdocs.org/sdr/ARWA20011116.md): Strap · cracked · Nov 20, 2001 · N1808E · Doug DC862 · Nacelle/Pylon, Main Frame
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND: NR 4 PYLON ACCESS DOOR 409 RT WITH TEMPORARY REPAIR, AFTER EVALUATION, FOUND CRACK ON OUTBOARD UPPER STRAP AT STA YUS 217. REPLACED STRAP IAW DC8 SRM 54-3-2,FIG 35, ITEM 5, NOTE 10. ACCOMPLISHED SB 54-70.
- [SDR ARWA20011107](https://openairdocs.org/sdr/ARWA20011107.md): Fitting · cracked · Nov 20, 2001 · N1808E · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPT STA 980 BULKHEAD LT STIFFENER WITH 1.5 INCH CRACK, NEAR MAIN CARGO DOOR COMPARTMENT FLOOR. REMOVED FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
- [SDR ARWA20011115](https://openairdocs.org/sdr/ARWA20011115.md): Stringer · Nov 20, 2001 · N1808E · Doug DC862 · Wing, Longeron/Stringer
  > N/R 1080 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH WING # 3 MAIN FUEL TANK INTERIOR BETWEEN STA. XRS 74 & SRS 107, STIFFENER 69 WITH 1.500" CRACK.CORRECTIVE ACTION: CUT-OUT DAMAGE SECTION OF STRINGER IAW DC8 SRM 57-2-2, PAGE 2, MADE SPLICE FIT
- [SDR ARWA20011114](https://openairdocs.org/sdr/ARWA20011114.md): Floorbeam · cracked · Nov 20, 2001 · N1808E · Doug DC862 · Fuselage Main, Floor Beam
  > DURING "C" CHECK INSPECTION, STA 1120, X=10 RT SIDE, FLOORBEAM WEB WITH CORROSION. ACCOMPLISHED HFEC INSPECTION IAW DC-8 NDT MANUAL CHAPTER 06, FOUND CRACK OF 0.562 INCHES LENGTH DUE TO CORROSION & MATERIAL LOSS. TRIMMED OUT DAMAGED AREA; FABRICATED FILLER A
- [SDR ARWA20011113](https://openairdocs.org/sdr/ARWA20011113.md): Skin Panel · Nov 20, 2001 · N1808E · Doug DC862 · Trailing Edge Flaps
  > N/R 1076 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH INBOARD FLAP LOWER SKIN WITH CRACK OF 0.500" BETWEEN STA. XW 92 & XW 104 FAIRING AREA.CORRECTIVE ACTION: REMOVED SKIN PANEL; FABRICATED NEW SKIN PANEL IAW AS ELEVEN INC. DWG # AS11321, SH 1 &
- [SDR ARWA20011112](https://openairdocs.org/sdr/ARWA20011112.md): Plate · Nov 20, 2001 · N1808E · Doug DC862 · Trailing Edge Flaps
  > N/R 1068 - DURING "C" CHECK, THE FOLLOWING WAS FOUND: LH WING I/B FLAP LOWER SKIN WITH DENT AT STA. XW L7.CORRECTIVE ACTION: FOUND DENT OUT OF LIMITS IAW DC8 SRM 57-1-0; REMOVED DAMAGED AREA; FABRICATED NEW SOLID PLATING, FILLER & SPLICE STRAP IAW AS ELEVEN IN
- [SDR ARWA20011111](https://openairdocs.org/sdr/ARWA20011111.md): Nozzle · cracked · Nov 20, 2001 · N1808E · Doug DC862 · Engine Collector/Tailpipe/Nozzle
  > DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: NR 4 ENGINE EXHAUST NOZZLE SPLITTER WITH CRACK AT 2 O'CLOCK. REMOVED SPLITTER; FABRICATED NEW SPLITTER IAW DC8 SRM 78-3-2, FIG 8, ITEM C. PRIMED AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-21.
- [SDR ARWA20011110](https://openairdocs.org/sdr/ARWA20011110.md): Fitting · Nov 20, 2001 · N1808E · Doug DC862 · Wing, Longeron/Stringer
  > N/R 440 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH WING # 4 ALT. TANK INTERIOR STA. XRS 408.00 STRINGER # 58 END FITTING WITH CRACK.CORRECTIVE ACTION: OPENED FUEL TANK PLATE IAW DC8 MM 57-30-0; REMOVED & REPLACED FITTINGS IAW DC8 SRM 51-1-20D AND C
- [SDR ARWA20011108](https://openairdocs.org/sdr/ARWA20011108.md): Plate · Nov 20, 2001 · N1808E · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > N/R 412 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH HORIZONTAL STABILIZER TIE STA. XE 77.000 AND 92.000 UPPER SKIN WITH INNER CORROSION.CORRECTIVE ACTION: REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED U
- [SDR ARWA20011106](https://openairdocs.org/sdr/ARWA20011106.md): Skin · corroded · Nov 20, 2001 · N1808E · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER T/E BETWEEN STA 175.000 & STA 190.000 UPPER SKIN WITH INNER CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED UPPER PLATING; FABRIC
- [SDR ARWA20011105](https://openairdocs.org/sdr/ARWA20011105.md): Plate · Nov 20, 2001 · N1808E · Doug DC862 · Elevator, Plate/Skin
  > N/R 192 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: LH ELEVATOR LWR SKIN WITH CORRUGATION & OIL CANNING IN SEVERAL POINTS, BETWEEN STA. XE 28.343 AND XE 200.218.CORRECTIVE ACTION: REMOVED LH ELEVATOR LWR PLATING; FABRICATED NEW PLATING IAW AS ELEVEN,
- [SDR ARWA0010603](https://openairdocs.org/sdr/ARWA0010603.md): Link Rod · defective · Jun 8, 2001 · N1808E · Doug DC862 · Landing Gear Door Retract Section
  > AFTER TAKEOFF OUT OF KMIA AND RAISED THE LANDING GEAR EXPERIENCED HEAVY NOSE VIBRATION. RECYCLED LANDING GEAR, BUT DID NOT HELP. DECLARED EMERGENCY AND LANDED OVERWEIGHT WITH FULL FLAPS. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NLG DOOR LT FW
- [SDR ARWA0010310](https://openairdocs.org/sdr/ARWA0010310.md): Guide · loose · Mar 30, 2001 · N1808E · Doug DC862 · Weather Radar System
  > RADAR WILL NOT PAINT WEATHER. AIRCRAFT DIVERTED TO MIAMI AND LANDED WITHOUT INCIDENT. TIGHTENED WAVE GUIDE; OPS CHECK NORMAL IAW MM 34-41-0.
- [SDR ARWA0010303](https://openairdocs.org/sdr/ARWA0010303.md): Tire · separated · Mar 6, 2001 · N1808E · Doug DC862 · Tire
  > AFTER TAKEOFF FROM KATL ATC ADVISED FLIGHT 509 THAT A TIRE WAS LEFT ON THE RUNWAY, FLIGHT CREW REPORTED THE INCIDENT TO MIAMI MX AND CONTINUE TO TJSJ. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT TJSJ. ON POST FLIGHT INSPECTION IT WAS C
- [SDR ARWA0010103](https://openairdocs.org/sdr/ARWA0010103.md): Bleed Valve · dirty · Jan 28, 2001 · N1808E · Doug DC862 · Compressor Bleed Valve
  > AT THE BEGINNING OF TAKEOFF ROLL NR 2 ENGINE HAD COMPRESSOR STALL. ENGINE PARAMETER WERE TAKEOFF, EPR WAS 1.88; DROPPED TO 1.75 N2 AND RECOVERED, FUEL FLOW DMI AND EGT WAS NORMAL. PERFORMED VISUAL CHECK AIR BLEED VALVE, CLEANED AND LUBRICATED IAW M/M 75-30-
- [SDR ARWA0010102](https://openairdocs.org/sdr/ARWA0010102.md): Ballast · smoke · Jan 25, 2001 · N1808E · Doug DC862 · Weather Radar System
  > DURING DESCENT, CO-PILOTS RADAR SCREEN HAD EVIDENCE OF SMOKE. TURNED OFF AND PULLED C/B. CHECKED WEATHER RADAR SYSTEM WIRING IAW W/D 34-10-0, FOUND NORMAL. GROUND OPERATIONAL CHECK IAW FDW M/M 34-41-0. NORMAL, NO TROUBLE FOUND. REF TO ITEM NR 1, FOUND EVID
- [SDR ARWA0001204](https://openairdocs.org/sdr/ARWA0001204.md): Switch · defective · Dec 23, 2000 · N1808E · Doug DC862 · Door Warning System
  > AFTER TAKE OFF KATL, DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED ABNORMAL PROCEDURE. UNABLE TO EXTINGUISH LIGHT; AIRCRAFT DIVERTED TO MIA & LANDED WITHOUT INCIDENTS.CORRECTIVE ACTION: REMOVED AND REPLACED LEFT AND RIGHT DOORS MICRO SWI
- [SDR 99T64R297AR](https://openairdocs.org/sdr/99T64R297AR.md): Skin · corroded · Aug 14, 1999 · N1808E · Doug DC862 · Wing, Plate/Skin
  > NR 0928 - PREVIOUS REPAIR SKIN CORRODED AND CORROSION EMANATING FROM UNDER REPAIR DOUBLER RIGHT WING UPPER SKIN STATION XW 50 STRINGER 11. REMOVED DOUBLERS. REMOVED CORROSION AND REINSTALLED DOUBLERS IAW BOEING MESSAGE M-7200-99-0228. ARROW AIR (M)
- [SDR 99T64R348AR](https://openairdocs.org/sdr/99T64R348AR.md): Duct · chafed · Jul 15, 1999 · N1808E · Doug DC862 · Air Distribution System
  > LEFT UPPER NOSE SECTION AC DUCT (HORSE SHOE) DUCT HAS HOLE CHAFFED IN IT. FABRICATED DOUBLER STRAP AND WELDED TO DUCT IAW BOEING MESSAGE M-7200-99-03383. (M)
- [SDR 99T64R344AR](https://openairdocs.org/sdr/99T64R344AR.md): Skin · dented · Jul 15, 1999 · N1808E · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING BOTTOM OUTBOARD OF RIGHT MLG PANEL DENTED IN TWO PLACES STATION XW90. NDT AREA, NO CRACKS NOTED, FILLED DENTS WIT HYSOL EA 934 NA, FABRICATED DOUBLER AND INSTALLED PER EO 99-061. (M)
- [SDR 99T64R358AR](https://openairdocs.org/sdr/99T64R358AR.md): Tube · loose · Jul 9, 1999 · N1808E · Doug DC862 · Airfoil Anti/De-ice System
  > LEFT NOSE SCOOP ANTI-ICE TUBE T PULLED LOOSE FROM DUCT OUTBOARD OF VALVE. REINSTALLED T AND WELDED PER EO 99-061. (M)
- [SDR 99T64R357AR](https://openairdocs.org/sdr/99T64R357AR.md): Tube · chafed · Jul 9, 1999 · N1808E · Doug DC862 · Airfoil Anti/De-ice System
  > RIGHT NOSE CHIN SCOOP ANTI-ICE TUBE T PULLED LOOSE AND CHAFFED HALF THROUGH O/B OF VALVE. WELDED CHAFFED AREA, REINSTALLED T TUBE AND WELDED PER EO 99-061. (M)
- [SDR 99T64R334AR](https://openairdocs.org/sdr/99T64R334AR.md): Tube · missing · Jul 8, 1999 · N1808E · Doug DC862 · Smoke Detection
  > FLT 2823 - CABIN SMOKE DETECTOR LINES AND END FITTINGS NOT INSTALLED. FABRICATED AND INSTALLED SMOKE DETECTOR TUBES AND FITTINGS IAW AS ELEVEN DWG AS 11045 WITH APPROVED FAA FORM 8110-3 DATED APRIL 27, 1999 APPROVED BY FAA ATLANTA CERTIFICATION OFFICE LETTER
- [SDR 99T64R350AR](https://openairdocs.org/sdr/99T64R350AR.md): Spar · cracked · Jul 7, 1999 · N1808E · Doug DC862 · Wing Spar
  > RIGHT WING LOWER FORWARD TANG OF FRONT SPAR OUTBOARD OF STATION XFS 515, 3 HOLES CRACKED. REMOVED NUT CHANNEL IAW DC-8 SRM 51-1-21. REAMED HOLES, EDDY CURRENT HOLES, NO DEFECTS. INSTALLED BUSHING IAW BOEING MESSAGE XXX-MEM-99-0007RR. (M)
- [SDR 99T64R370AR](https://openairdocs.org/sdr/99T64R370AR.md): Duct · worn · Jul 7, 1999 · N1808E · Doug DC862 · Engine Start Valves/Controls
  > NR 2 ENGINE STARTER SUPPLY DUCT BADLY WORN. WELDED DUCT IAW BOEING MESSAGE M7200-99-05-0359. (M)
- [SDR 99T64R343AR](https://openairdocs.org/sdr/99T64R343AR.md): Guide · broken · Jul 7, 1999 · N1808E · Doug DC862 · Leading Edge Slat Control System
  > RIGHT WING INBOARD LEADING EDGE OUTBOARD END HAS CABLE GUIDE (PHENOLIC BLOCK) BROKEN. APPLIED EPOXO 88 TWO PART EPOXY WITH AN ADDITIONAL 4 FASTENERS PER EO 99-061. (M)
- [SDR 99T64R386AR](https://openairdocs.org/sdr/99T64R386AR.md): Fitting · damaged · Jul 7, 1999 · N1808E · Doug DC862 · Trailing Edge Flaps
  > NR 2579 - REMOVE FLAP CANOE FITTING AT STATION XF340, HOLE ELONGATED. REMOVED FLAP CANOE FITTING AT STATINO XF340 IAW DC-8 MM 27-51-12. REPLACED FLAP CANOE FITTING IAW DC-8 MM 27-51-12, SB27-260 R2 AND BOEING MESSAGE M-72-99-04220. (M)
- [SDR T64R387AR](https://openairdocs.org/sdr/T64R387AR.md): Cover · punctured · Jul 5, 1999 · N1808E · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > ARROW AIR - NR 2073, LEFT HORIZ STABILIZER T/E OUTBOARD DAMPER WELL HOLE PUNCHED THROUGH. REMOVED DAMPER WELL COVER IAW DC-8 SRM 51-1-21, WELDED HOLE PER EO 99-061 AND REINSTALLED IAW DC-8 SRM 51-1-21. (M)
- [SDR 99T64R283AR](https://openairdocs.org/sdr/99T64R283AR.md): Duct · cracked · Jun 25, 1999 · N1808E · Doug DC862 · Engine Oil Cooler
  > NR 3050 - NR 3 TURBO COMPRESSOR OIL COOLING DUCT CRACKED. WELDED CRACK IAW BOEING MESSAGE M-7200-99-05081. ARROW AIR (M)
- [SDR 99T64R258AR](https://openairdocs.org/sdr/99T64R258AR.md): Duct · cracked · Jun 25, 1999 · N1808E · Doug DC862 · Engine Oil Cooler
  > NR 0161 - CSD OIL COOLER DUCT CRACKED AT FORWARD MOUNTING FLANGE ENG S/N 670982 NR 4 POSITION. WELDED CRACK IAW BOEING ENGINEERING MESSAGE M-7200-99-05081 WITH APPROVED FAA FORM 8110-3 DATED 6-21-99. REF: ARROW AIR, ARWA. (X)
- [SDR 99T64R367AR](https://openairdocs.org/sdr/99T64R367AR.md): Panel · corroded · Jun 24, 1999 · N1808E · Doug DC862 · Leading Edge Devices
  > RIGHT OUTBOARD INBOARD SLOT PANEL HAS CORROSION XS 442.185. REMOVED CORROSION AND BLENDED AREA IAW EO 99-061. (M)
- [SDR 99T64R243AR](https://openairdocs.org/sdr/99T64R243AR.md): Access Door · cracked · Jun 17, 1999 · N1808E · Doug DC862 · Accessory Compartment Doors
  > NR 1066 - ACCESS DOOR STA 1380 BENT AND CRACKED (PLEXIGLASS CRACKED). FABRICATED NEW ACCESS DOOR PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-10-99. REF: ARROW AIR, ARWA. (X)
- [SDR 99T64R341AR](https://openairdocs.org/sdr/99T64R341AR.md): Angle · misinstalled · Jun 15, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR UPPER JAM INSTALLATION Z ANGLE INCORRECTLY INSTALLED STATION 450. DOES NOT EFFECT THE INTEGRITY OF THE DOOR. NO CORRECTIVE MEASUREMENTS NECESSARY IAW DWG AS11048. (M)
- [SDR 99T64R241AR](https://openairdocs.org/sdr/99T64R241AR.md): Frame · cracked · Jun 15, 1999 · N1808E · Doug DC862 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 0762 - 6 INCH CRACK IN NR 3 PYLON CAP FORMER (HORSE COLLAR) FORWARD SECTION STA YN161. FABRICATED REPLACMENT PART PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR - ARWA. (X)
- [SDR 99T64R383AR](https://openairdocs.org/sdr/99T64R383AR.md): Skin · gouged · Jun 9, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/Skin
  > NR 0907 D-PIT DOOR CUTOUT - SKIN FORWARD LOWER EDGE GOUGED. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED PER EO 99-048 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED JUNE 14, 1999. REF: ARROW AIR, ARWA. (X)
- [SDR 99T64R252AR](https://openairdocs.org/sdr/99T64R252AR.md): Skin · damaged · Jun 9, 1999 · N1808E · Doug DC862 · Trailing Edge Flaps
  > NR 2392 - LEFT INBOARD FLAP WEDGE, DAMAGED SKIN LOWER STA XW 47. FABRICATED NEW LOWER SKIN LEFT INBOARD FLAP WEDGE PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X)
- [SDR 99T64R349AR](https://openairdocs.org/sdr/99T64R349AR.md): Duct · chafed · Jun 7, 1999 · N1808E · Doug DC862 · Engine Start Valves/Controls
  > HEAVY CHAF MARK NR 3 ENGINE STARTER DUCT 10 OCL POS. FABRICATED DOUBLERS AND WELDED ON DUCT IAW BOEING MESSAGE M-7200-99-04226. (M)
- [SDR 99T64R346AR](https://openairdocs.org/sdr/99T64R346AR.md): Angle · damaged · Jun 7, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous Structure
  > CLEAN INSPECT REPAIR AS NECESSARY ALL SIDE RAIL SYSTEM. CUT OUT DAMAGED AREAS FABRICATED ANGLE TIERNAY AND INSTALLED PER AS 11040. (M)
- [SDR 99T64R337AR](https://openairdocs.org/sdr/99T64R337AR.md): Beam · mismanufactured · Jun 7, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR JAM AFT JAM AFT BEAM INBOARD LEAG TO SHORT. FABRICATED DOUBLER SHIM/SPACER IAW EO DWG AS 11042. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW EO AS11042 AND DC-8 SRM 51-1-21 WITH APPROVED FAA FORM 8110-3 DATED MAY 12, 1999. (M)
- [SDR 99T64R336AR](https://openairdocs.org/sdr/99T64R336AR.md): Beam · short · Jun 7, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous Structure
  > FLT 2851 - MAIN CARGO DOOR FORWARD JAMB - FORWARD BEAM INBOARD LEG TOO SHORT. FABRICATED DOUBLER SHIMS IAW EO DWG AS11042, TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW EO DWG AS11042 AND DC-8 SRM 51-1-21. WITH APPROVED FAA FORM 8110-3 DATED MAY 1
- [SDR 99T64R265AR](https://openairdocs.org/sdr/99T64R265AR.md): Spar · corroded · Jun 7, 1999 · N1808E · Doug DC862 · Wing Spar
  > NR 2841 - LT WING REAR SPAR HAS 4 EACH AREAS OF CORROSION BETWEEN XRS 139-172. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPECIAL WASHERS AND DOUBLER, INSTALLED PER EO 99-061 WITH APPROVEDF FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)
- [SDR 99T64R345AR](https://openairdocs.org/sdr/99T64R345AR.md): Spar · corroded · Jun 4, 1999 · N1808E · Doug DC862 · Wing Spar
  > LT WING AFT SPAR HAS 7 EACH AREAS OF CORROSION AT XRS 190. REMOVED CORROSION, FABRICATED SPECIAL WASHERS AND DOUBLERS AND INSTALLED PER EO 99-061. (M)
- [SDR 99T64R368AR](https://openairdocs.org/sdr/99T64R368AR.md): Door · corroded · Jun 3, 1999 · N1808E · Doug DC862 · Emergency Exits
  > FORWARD RIGHT O/W EXIT DOOR CORROSION WINDOW FRAME INTERNAL STATION 730. REMOVED CORROSION FILLED WITH HYSOL EA 9309NA. FAIRED TO ORIGINAL THICKNESS. TREATED AND FINISHED IAW DC-8 SRM 51-1-8 PER EO NR 99-061. (M)
- [SDR 99T64R260AR](https://openairdocs.org/sdr/99T64R260AR.md): Window Frame · corroded · Jun 3, 1999 · N1808E · Doug DC862 · Emergency Exits
  > NR 2633 - AFT LT OVER WING DOOR, WINDOW FRAME CORRODED STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL 9309NA, FAIR TO ORIGINAL THICKNESS, TREATED AND PRIMED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARRO
- [SDR 99T64R251AR](https://openairdocs.org/sdr/99T64R251AR.md): Window Frame · corroded · Jun 3, 1999 · N1808E · Doug DC862 · Emergency Exits
  > NR 2286 - FORWARD LT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 717-742. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO FRAME, FAIRED TO ORIGINAL THICKNESS OF FRAME. TREATED AND PRIMED PER EO 99-061 WITH APPROVED FAA FORM 8110
- [SDR 99T64R250AR](https://openairdocs.org/sdr/99T64R250AR.md): Window Frame · corroded · Jun 3, 1999 · N1808E · Doug DC862 · Emergency Exits
  > NR 2285 - AFT RIGHT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO FRAME, FAIRED TO ORIGINAL THICNESS OF FRAME. TREATED AND PRIMES PER EO 99-061 WITH APPROVED FAA F
- [SDR 99T64R269AR](https://openairdocs.org/sdr/99T64R269AR.md): Floorbeam · corroded · Jun 2, 1999 · N1808E · Doug DC862 · Fuselage Main, Floor Beam
  > NR 2958 - CORROSION BLISTER AFT SIDE CABIN FLOORBEAM STA 1120 RBL 34 INCHES. REMOVE CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED PER EO 99-016 WITH APPROVED FAA FORM 8110-3 DATED 6-7-99. REF: ARROW AIR, ARWA. (X)
- [SDR 99T64R267AR](https://openairdocs.org/sdr/99T64R267AR.md): Nutplate · missing · Jun 2, 1999 · N1808E · Doug DC862 · Wing Miscellaneous Structure
  > NR 288 - TWO EACH, CHANNEL NUTPLATES AND SCREWS MISSING LT INBOARD L/E FUEL TANK XRS 64-XFS 14. INSTALLED NAS-1670-4 BLIND FASTENERS PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)

Next page: https://openairdocs.org/deregistered/N1808E-2017-03-10/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 = 'N1808E' AND deregistration_id = 'N1808E-2017-03-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N1808E-2017-03-10/reports

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