# Service difficulty reports: N802BN, cancelled Jun 19, 2006

A list on [N802BN, cancelled Jun 19, 2006](https://openairdocs.org/deregistered/N802BN-2006-06-19.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 · 88 reports

- [SDR ARWA20030708](https://openairdocs.org/sdr/ARWA20030708.md): Floorbeam · corroded · Jul 22, 2003 · N802BN · Doug DC862 · Fuselage Main, Floor Beam
  > DURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT STATION 1520, RBL 32 FLOORBEAM UPPER FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM UPPER AFT FLANGE AT STATION 1520 RBL 32 IAW AVITAS ENGINEERING ORDER AROW-034RO-1, PAGES 1 TO
- [SDR ARWA20030605](https://openairdocs.org/sdr/ARWA20030605.md): Door Frame · cracked · Jun 5, 2003 · N802BN · Doug DC862 · Fuselage Main, Structure
  > DURING MAINTENANCE INSPECTION THE FOLLOWING WAS FOUND, FORWARD ENTRY DOOR FRAME, BOTTOM AFT CORNER HFEC INSPECTION REVEALED.1250 INCH CRACK. ACCOMPLISHED REPAIRS AT FORWARD ENTRY DOOR AFT LOWER CORNER IAW SB 53-075 AND DRAWING NR SR08530021.
- [SDR ARWA20030402](https://openairdocs.org/sdr/ARWA20030402.md): Rotary Actuator · jammed · Apr 11, 2003 · N802BN · Doug DC862 · Stabilizer Actuator
  > RIGHT SUIT CASE HANDLE JAMMED IN FORWARD POSITION AND COULD NOT BE MOVED EVEN WITH C/B PULLED. REMOVED AND REPLACED RIGHT LONGITUDINAL TRIM SERVO ACTUATOR IAW MM 27-41-10. OPERATIONAL CHECK NORMAL IAW MM 27-40-0.
- [SDR ARWA20030301](https://openairdocs.org/sdr/ARWA20030301.md): Hose · leaking · Mar 9, 2003 · N802BN · Doug DC862 · Hydraulic System, Main
  > IN FLIGHT LOSS OF HYDRAULIC QUANTITY OF PRESSURE; PERFORMED APPROACH CHECKLIST. FOUND HYDRAULIC PRESSURE HOSE LEAKING AT NR 2 ENGINE. REMOVED AND REPLACED HYDRAULIC HOSE ON HYDRAULIC PUMP IN ACCORDANCE WITH MM 20-12-0. SERVICE HYDRAULIC RESERVOIR IAW MM 12
- [SDR ARWA20030102](https://openairdocs.org/sdr/ARWA20030102.md): Valve · inoperative · Jan 19, 2003 · N802BN · Doug DC862 · Landing Gear Brake System
  > DURING TAXI, BEFORE TAKEOFF, ANTI SKID INOPERATIVE LIGHT ON WITH SWITCH IN (ON) POSITION. REMOVED AND REPLACED RT MAIN LANDING GEAR OUTBOARD ANTI SKID DUAL SERVO VALVE. BLED SYSTEM, OPS CHECKED AND FOUND NORMAL IAW MM.
- [SDR ARWA20021203](https://openairdocs.org/sdr/ARWA20021203.md): Hose · damaged · Dec 11, 2002 · N802BN · Doug DC862 · Hydraulic System, Main
  > LOST HYDRAULIC QUANTITY TOP OF DESCEND FOLLOWED BY ABNORMAL CHECKLIST AND PROCEDURES. CORRECTIVE ACTION: FOUND HYDRAULIC HOSE FROM PUMP ENGINE NR 2 DAMAGE. REMOVED AND REPLACED HOSE IAW MM, OPERATIONS CHECK OK IAW MM.
- [SDR ARWA20021108](https://openairdocs.org/sdr/ARWA20021108.md): Cylinder · inoperative · Nov 20, 2002 · N802BN · Doug DC862 · Landing Gear Retraction/Extension System
  > IN FLIGHT, AFTER NORMAL GEAR RETRACTION, RED GEAR LIGHT ON AFTER UP LATCH CHECK. FOLLOWED ABNORMAL CHECKLIST. REMOVED AND REPLACED LEFT GEAR UP LATCH CYLINDER IAW MM, REMOVED AND REPLACED LEFT GEAR ACTUATING CYLINDER IAW MM. PERFORMED CHECK, NO LEAK, GOOD.
- [SDR ARWA20021106](https://openairdocs.org/sdr/ARWA20021106.md): Engine · failed · Nov 14, 2002 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)
  > AT 2130Z, NR 2 OIL QUANTITY RAPIDLY DROPPED TO 1 GALLON, SUBSEQUENTLY OIL PRESSURE DROPPED TO 5 PSI AND OIL PRESSURE LOW LIGHT ILLUMINATED. PERFORMED IN FLIGHT ENGINE SHUTDOWN PROCEDURE IAW ABNORMAL CHECKLIST, WINDMILLING OIL PRESSURE. REMAINED AT 5 PSI. INS
- [SDR ARWA20021105](https://openairdocs.org/sdr/ARWA20021105.md): Receiver · inoperative · Nov 13, 2002 · N802BN · Doug DC862 · Localizer/VOR System
  > NR 2 VHF FIRST OFFICER SIDE COURSE DEVIATION INDICATOR INOPERATIVE, RETURNED TO MIAMI. REMOVED & REPLACED NR 2 VOR INSTRUMENT LANDING SYSTEM RECEIVER. SYSTEM OPERATIONS NORMAL IAW MM 34-52-0. AIRCRAFT RETURNED TO SERVICE.
- [SDR ARWA20021102](https://openairdocs.org/sdr/ARWA20021102.md): Heat Exchanger · failed · Nov 7, 2002 · N802BN · Doug DC862 · Engine Oil Temperature
  > NR 1 ENGINE OIL TEMPERATURE INDICATED 140 DEGREES FOR 15 MINUTES; THEN WENT TO 150 DEGREES THROTTLE IDLE, ALL OTHER PARAMETERS NORMAL, PERFORMED IN FLIGHT ENGINE SHUTDOWN CHECKLIST. WITH NR 1 ENGINE SHUTDOWN, OIL PRESSURE AT 20 PSI AND TEMPERATURE 60 DEGREES
- [SDR ARWA20021004](https://openairdocs.org/sdr/ARWA20021004.md): Engine · malfunctioned · Oct 12, 2002 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)
  > DURING CRUISE NR 3 ENGINE IDLE PRESS. LIGHT ILLUMINATED. OIL PRESS. 25 PSI, QTY, 1 GALLON. TEMP 135 DEGREES. ENGINE SHUT DOWN AT 1421Z. WINDMILLING OIL PRESSURE ZERO. REMOVED ENGINE, AND REPLACE WITH SERVICEABLE ENGINE. FUNCTIONAL TEST AND GROUND RUN-
- [SDR ARWA20020901](https://openairdocs.org/sdr/ARWA20020901.md): Cylinder · leaking · Sep 2, 2002 · N802BN · Doug DC862 · Landing Gear Retraction/Extension System
  > AFTER LANDING IN SKCL LOSS OF HYDRAULICS PRESSURE AND QUANTITY. FOUND HYDRAULIC LEAK IN LEFT BOGIE TRIM CYLINDER. REMOVED AND REPLACED LEFT HYDRAULIC BOGIE TRIM CYLINDER AS PER ALTERNATE METHOD MM REF 32-33-1. SERVICED HYDRAULIC IAW MM 12-30-1 AND BLEED SYS
- [SDR ARWA20020203](https://openairdocs.org/sdr/ARWA20020203.md): Fitting · cracked · Feb 4, 2002 · N802BN · Doug DC862 · Wing Miscellaneous Structure
  > DURING C-CHECK, RIGHT WING NR 4 ALTERNATE FUEL TANK INTERIOR S-58 END FITTING WITH 1 INCH CRACK AT STA XRS 408.00.
- [SDR ARWA20020202](https://openairdocs.org/sdr/ARWA20020202.md): Fitting · cracked · Feb 4, 2002 · N802BN · Doug DC862 · Wing Miscellaneous Structure
  > DURING C-CHECK, LT WING NR 1 ALTERNATE FUEL TANK INTERIOR S-57 END FITTING WITH 1 INCH CRACK STA XRS 408.00. REMOVED AND REPLACED STRINGER END FITTINGS IAW DC-8 SRM 51-1-20D.
- [SDR ARWA20011212](https://openairdocs.org/sdr/ARWA20011212.md): Bleed Valve · lack of lube · Dec 23, 2001 · N802BN · Doug DC862 · Compressor Bleed Valve
  > NR 3 ENGINE COMPRESSOR STALL AT BRAKE RELEASE MAX POWER 1.89 EPR RETURN TO RAMP FOR CKV & FOR NOTE 13 DEGREE CELSIUS ENGINE ANTI ICE OFF AND NO WIND. LUBED SURGE BLEED VALVE IAW MM 75-30-3, SYSTEM OPS CKD NORMAL IAW MM 71-00 ENGINE RUN. AIRCRAFT RETURNED TO
- [SDR ARWA0011014](https://openairdocs.org/sdr/ARWA0011014.md): Pump · leaking · Nov 9, 2001 · N802BN · Doug DC862 · Hydraulic Pump (Electric/Engine), Main
  > IN CRUISE, HYDRAULIC QUANTITY DROPPED SLIGHTLY ABOVE EMERGENCY LEVEL. PERFORMED LOSS OF HYDRAULIC PRESSURE ABNORMAL EMERGENCY CHECKLIST. FLIGHT RESTRICTED TO MACH.65 AND 230 KIAS. CONTINUED WITHOUT INCIDENT. AFTER LANDING, MX FOUND AUX RUDDER PUMP LEAKING
- [SDR ARWA0010803](https://openairdocs.org/sdr/ARWA0010803.md): Seal · Aug 7, 2001 · N802BN · Doug DC862 · Engine Oil System (Airframe Furnished)
  > LOG PAGE 53334. DISCREPANCY: ON FINAL APPROACH SHUT DOWN #3 ENGINE DUE TO RAPID DROP IN OIL QUANTITY AND PRESSURE. CORRECTIVE ACTION: REMOVED HOUSING AND SEAL FROM FUEL BOOST PUMP DRIVE ON # 3 ENGINE GEAR BOX. INSTALLED SEAL (SEAL P/N 730376) AND HOUSING
- [SDR ARWA0010403](https://openairdocs.org/sdr/ARWA0010403.md): Generator · malfunctioned · Apr 7, 2001 · N802BN · Doug DC862 · AC Generator-Alternator
  > NR 2 GENERATOR FIELD RELAY TRIPS AND WILL NOT RESET.CORRECTIVE ACTION: REMOVED AND REPLACED NR 2 GENERATOR OPERATIONAL CHECK NORMAL DURING RUN UP IAW MM 24-20-1 & 71-00
- [SDR ARWA1000204](https://openairdocs.org/sdr/ARWA1000204.md): O-Ring · torn · Feb 25, 2001 · N802BN · Doug DC862 · Hydraulic System, Main
  > HYDRAULIC SYSTEM LOSS DOWN TO STADPIPE, EMERGENCY CHECK, LIST C/W. RETURNED TO STATION. FOUND O-RING FROM RT AILERON ACTUATOR TUBING FITTING LEAKING. REPLACED O-RING IAW MM 20-60-0, OPS CHECK NORMAL. NO LEAKS NOTED, SYSTEM CHECK SATISFACTORY.
- [SDR ARWA0010203](https://openairdocs.org/sdr/ARWA0010203.md): Link · broken · Feb 7, 2001 · N802BN · Doug DC862 · Trailing Flap Position Indicating System
  > FLAP IND HAS SPLIT NEEDLES. FOUND LEFTI/B FLAP LINK BROKEN ON THE O/B HINGE. REMOVED AND REPLACED WITH NEW P/N 5751152-501. REFERENCE MM 27-51-4. OPS CHECK SATISFACTORY.
- [SDR ARWA991001](https://openairdocs.org/sdr/ARWA991001.md): Fire Loop · failed · Oct 16, 1999 · N802BN · Doug DC862 · Fire Detection
  > MIA - FLT 447 - AT 14,000 FT ALT, NR 1 ENGINE FIRE WARNING SOUNDED. ENGINE SHUTDOWN. OIL QTY AND OIL PRESSURE NORMAL AND OIL TEMP HIGH AT 140 DEGREES. REMOVED AND REPLACED NR 1 ENGINE MAIN OIL SCREEN. NO CONTAMINATION FOUND. REMOVED DISCHARGED FIRE BOTTLE
- [SDR ARWA990704](https://openairdocs.org/sdr/ARWA990704.md): Structure · cracked · Jul 27, 1999 · N802BN · Doug DC862 · Fuselage Main, Structure
  > MIA - FLT 574 - DURING ROUTINE INSPECTION DURING MAIN CARGO DOOR MAINTENANCE, DETECTED APPROXIMATELY 10 INCH CRACK IN STC DOUBLER EMANATING LOWER FORWARD CORNER AT CUSP LINE. AFTER GAINING INTERNAL ACCESS TO AREA, FOUND 5 EACH FLOORBEAM TO LOWER SILL FITTINGS
- [SDR ARWA990602](https://openairdocs.org/sdr/ARWA990602.md): Engine · failed · Jun 22, 1999 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)
  > SJU - FLT 601 - CLIMBING-OUT THROUGH 16000 FT AT 1302Z, NR 4 ENGINE LOUD BANG ALL PARAMETERS ERRATIC. COMPLETED APPROPRIATE CHECK LISTS. DUMPED FUEL TO MAX LANDING WEIGHT. RETURNED TO TJSJ WITHOUT INCIDENT. CUASE OF FAILURE CONTINUES. REMOVAL AND REPLACEME
- [SDR ARWA990502](https://openairdocs.org/sdr/ARWA990502.md): Bracket · broken · May 23, 1999 · N802BN · Doug DC862 · Nacelle/Pylon Structure
  > BOG - FLT 709 - NR 1 ENGINE INBOARD BYPASS AIR CONSTANT DUCT STRAP BRACKET BROKEN. BLOWOUT DOOR LOST IN FLIGHT. REMOVED AND REPLACED STRAP. REPLACED NR 1 ENGINE. COWL BLOWOUT DOOR. ENGINE IDLE RUN CHECK OK. (M)
- [SDR ARWA990304](https://openairdocs.org/sdr/ARWA990304.md): Wheel · failed · Mar 6, 1999 · N802BN · Doug DC862 · Wheel/Ski/Float
  > MIA - FLT 807 - BLOCK TURN BACK, AT THE BEGINNING OF TAKEOFF HEARD A LOUD NOISE FROM LEFT MLG WHEEL WELL. RETURNED TO RAMP. MAINTENANCE FOUND NR 6 MLG WHEEL INBOARD HALF FLANGE HAD SEPARATED AND TIRE WAS MISSING. WHEEL PARTS AND TIRE WERE RECOVERED. NR 6 M
- [SDR ARWA990203](https://openairdocs.org/sdr/ARWA990203.md): Light · malfunctioned · Feb 12, 1999 · N802BN · Doug DC862 · Landing Gear Position and Warning
  > MIA - LANDING GEAR DOOR NOT LATCHED. REMAINED ON, WARNING LIGHT ILLUMINATED. AFTER ALL ABNORMAL PROCEDURES WERE PERFORMED. RETURNED TO MIAMI WITHOUT INCIDENT. T/S FOUND DOOR NOT LATCHED WARNING LIGHT SOCKET DAMAGE. REMOVED AND REPLACED ELECTRICAL SOCKET I
- [SDR 99T64R063AR](https://openairdocs.org/sdr/99T64R063AR.md): Frame · corroded · Feb 5, 1999 · N802BN · Doug DC862 · Fuselage Main, Frame
  > FUSELAGE LONGERON 25L FRAME 119L FINGER DOUBLER AT FLOORBEAM COCKPIT SUB FLOOR CORROSION EXFOLIATION. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND INSTALLED PER EO DRAWING NR 99-006 WITH 8110-3 DATED 0/21/99. (M)
- [SDR 99T64R062AR](https://openairdocs.org/sdr/99T64R062AR.md): Frame · corroded · Feb 2, 1999 · N802BN · Doug DC862 · Fuselage Main, Frame
  > FUSELAGE STATION 148 LEFT SIDE FUSELAGE SUB FLOOR FRAME ATTACH ANGLE CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, AND INSTALLED PER EO DRAWING NR 99-009 AND 8110-3 DATED 01/12/99. (M)
- [SDR ARWA990106](https://openairdocs.org/sdr/ARWA990106.md): Engine · leaking · Jan 12, 1999 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)
  > MIA - FLT 1628 - FL310, OIL QTY NR 1 ENGINE DROPPED TO.5 GALLON, OK OIL AND SUBSEQUENT ENGINE DAMAGE. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AS EPR ABNORMAL CHECKLIST. AFTER SHUTDOWN, N1 25 PERCENT, N2 40 PERCENT, OIL PRESS 21 PSI. REMOVED OIL SCREEN AND
- [SDR ARWA990105](https://openairdocs.org/sdr/ARWA990105.md): Bolt · worn · Jan 10, 1999 · N802BN · Doug DC862 · Aileron Control System
  > MIA - FLT 9627 - ON PRE-FLIGHT, FOUND RT AILERON INBD TO OTBD SECTION 2 INCH SPLIT. TROUBLESHOT, FOUND EYE BOLT ATTACHING INBD/OTBD AILERON LOOSE AND WORN. REPLACED SAME IAW 211-11-02. OPERATIONAL PER MM 27-11-02. (X)
- [SDR ARWA981211](https://openairdocs.org/sdr/ARWA981211.md): Pitot Tube · inop · Dec 19, 1998 · N802BN · Doug DC862 · Pitot/Static Anti-Ice System
  > F/O PITOT HEAT INOP. REMOVED AND REPLACED CURRENT DETECTOR IAW DC-8 M/M 30-30-0. NO HELP. REMOVED AND REPLACED F/O PITOT TUBE IAW DC-8 M/M 30-30-0. PERFORMED PITOT STATIC LEAK CHECK IAW DC-8 M/M 34-12-0. OPERATION NORMAL.
- [SDR ARWA981104](https://openairdocs.org/sdr/ARWA981104.md): Connector · loose · Nov 18, 1998 · N802BN · Doug DC862 · Engine EGT/TIT Indicating System
  > NR 1 EGT FLUCTUATING AT 300 DEGREES, ADVANCING THROTTLE ON T/O ROLL. ABORTED T/O AND RETURNED TO RAMP. TIGHTEN CANNON PLUG ON EGT INDICATOR, OPS CHECKED NORMAL IAW M/M 77-20-00.
- [SDR ARWA980911](https://openairdocs.org/sdr/ARWA980911.md): Fitting · loose · Sep 22, 1998 · N802BN · Doug DC862 · Turbine Engine Oil System
  > TUS - SHUTDOWN NR 4 ENGINE S/N 671443 AT 1345Z DUE TO STEADY OIL PRESS LIGHT AND INDICATED PRESS LESS THAN 35 PSI. WINDMILLING PRESS AT 18 PSI. TIGHTENED LOOS SWIVEL FITTING AT NR 6 BEARING INLET. ENGINE RUN UP. NO LEAKS NOTED. (M)
- [SDR ARWA980910](https://openairdocs.org/sdr/ARWA980910.md): Spar · cracked · Sep 19, 1998 · N802BN · Doug DC862 · Wing Spar
  > RT WING FRONT SPAR LOWER CAP HAS TWO ADJACENT ATTACHMENT HOLES CRACKED BETWEEN STA XFS 515.000 AND XFS 526.760. CUT OUT DAMAGED AREA PER DRA J060232, FABRICATED FILLER, ANGLES AND DOUBLER PER DRG J060232 AND ROD SKETCH 97-02-10-005. LOCATED, DRILLED AND STR
- [SDR ARWA980803](https://openairdocs.org/sdr/ARWA980803.md): Nut · loose · Aug 5, 1998 · N802BN · Doug DC862 · Hydraulic System, Main
  > KELP - FLT 045 - DURING CLIMB-OUT, HYDRAULIC FLUID LOSS, PRESSURE FLUCTUATING, EMERGENCY CHECK LIST COMPLETED, 6 GALLONS REMAINING. RETURNED TO KELP. TIGHTENED LOOSE B-NUT ON RT AILERON ACTUATOR SWIVEL GLAND NUT, LEAK AND OPS CHECK NORMAL IAW 27-10-0. HYDRA
- [SDR ARWA9807131](https://openairdocs.org/sdr/ARWA9807131.md): Connector · loose · Jul 30, 1998 · N802BN · Doug DC862 · Landing Gear Door Retract Section
  > DAY - FLT 046 - AFTER TAKEOFF, GEAR DOOR NOT LATCH LIGHT ILLUMINATED, ABNORMAL CHECK LIST COMPLETED. DOOR NOT LATCH LIGHT REMAINED ILLUMINATED. RETURNED TO DAY, FUEL DUMPED APPROX 4,000 POUNDS. RESECURED CANNON PLUG ON LT MAIN DOOR SWITCH, CYCLED SYSTEM IAW
- [SDR ARWA9807127](https://openairdocs.org/sdr/ARWA9807127.md): Cooling Valve · miswired · Jul 17, 1998 · N802BN · Doug DC862 · Air Distribution System
  > AIRCRAFT CABIN ALT AT 9000 AND CLIMBING WITH 3 T/C'S OPERATING AT 31,000 FOUND RADIO RACK COOLING VALVE OPEN WHEN AIRBORNE. CORRECTED WIRING AT RELAY R2-64, OPS NORMAL IAW MM 21-50-0. PRESSURIZATION NORMAL ON RUN-UP IAW MM 21-30-0.
- [SDR ARWA9807126](https://openairdocs.org/sdr/ARWA9807126.md): B-Nut · loose · Jul 17, 1998 · N802BN · Doug DC862 · Pitot/Static System
  > 30 KNOT SPLIT ON AIRSPEED AND 1000 SPLIT ON ALTIMETERS CLIMBING THROUGH FL 310, SPLITS ON BOTH WERE INCREASING, BOTH HIGH ON F/O SIDE. SECURED LOOSE B NUT IN CEILING OF AIRCRAFT BELLY. ACCOMPLISHED PITOT-STATIC CHECK. OPS AND LEAK CHECK ED NORMAL IAW MM 34-
- [SDR ARWA9807125](https://openairdocs.org/sdr/ARWA9807125.md): Support · corroded · Jul 17, 1998 · N802BN · Doug DC862 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CROSS BEAM AT STATION 1540 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IN ACCORDANCE WITH JOSSAIR, CO EO NR 18R537001. WORK ACCOMPLISHED UNDER ARROW AIR, INC FORM JW3B, WORK ORDER NR 980802, CONTROL NR 5006.
- [SDR ARWA9807124](https://openairdocs.org/sdr/ARWA9807124.md): Bulkhead Bracket · cracked · Jul 17, 1998 · N802BN · Doug DC862 · Fuselage Main, Bulkhead
  > BOTH ATTACH BRACKETS HOLDING PRESS. SEALS TRUMPETS ARE CRACKED AT AFT PRESSURE BULKHEAD AREA. FABRICATED REPAIR AND INSTALLED IN ACCORDANCE WITH JOSSAIR, CO EO NR18R539001. WORK ACCOMPLISHED UNDER ARROW AR FORM JW3B, WORK ORDER 980802, CONTROL NR 5009.
- [SDR ARWA980508](https://openairdocs.org/sdr/ARWA980508.md): Swivel · leaking · Jun 3, 1998 · N802BN · Doug DC862 · Aileron Tab Control System
  > ON LANDING ROLL, NOTICED HYD QUANTITY DECREASING DOWN TO STAND PIPE. REMOVED AND REPLACED AILERON TAB LOCK OUT CYLINDER SWIVEL GLAND IAW MM 27-11-7, OPERATION LEAK CHECK NORMAL.
- [SDR ARWA980409](https://openairdocs.org/sdr/ARWA980409.md): Cowling · damaged · Apr 27, 1998 · N802BN · Doug DC862 · Engine Cowling System
  > DURING GROUND HANDLING, NR 2 ENGINE COWLING DAMAGED BY BELT LOADER, LT AND RT FWD COWLINGS. LT AND RT AFT COWLINGS AND T/R LOWER STRINGER, REMOVED AND REPLACED NR 2 ENGINE. FWD AND AFT COWLINGS AND T/R LOWER STRINGER AS PER DC-8 MM 71-10-2 AND 78-30-0.
- [SDR ARWA980311](https://openairdocs.org/sdr/ARWA980311.md): Duct · failed · Mar 31, 1998 · N802BN · Doug DC862 · Cabin Compressor System
  > AT 39,000 LOSS PRESSURIZATION, PROCED FOR EMERGENCY DESCENT. RETURNED TO MIAMI. AT ARRIVAL AIRCRAFT WILL NOT ACCEPT EXTERNAL POWER. FOUND CLAMP TO NR 3 T/C DUCT HAD FAILED, CAUSING DUCT TO COME LOOSE. RESECURED DUCT WITH NEW CLAMP AND PERFORMED OPS CHECK O
- [SDR ARWA980308](https://openairdocs.org/sdr/ARWA980308.md): Wingtip · damaged · Mar 24, 1998 · N802BN · Doug DC862 · Wing Miscellaneous Structure
  > ON RAMP, WHILE BEING MANSHALLED INTO THE RAMP, THE LEFT WING TIP MADE CONTACT WITH ANOTHER AIRCRAFT. TEMPORARY REPAIR ACCOMPLISHED IAW MM 6 PAR 5-1 TO FLY A/C BACK TO MIAMI. REMOVED AND REPLACED DAMAGED WING TIP IAW SRM 51-30-00.
- [SDR ARWA980203](https://openairdocs.org/sdr/ARWA980203.md): Control Box · failed · Feb 2, 1998 · N802BN · Doug DC862 · Brake Anti-Skid Section
  > AFTER T/O, ANTI-SKID LIGHT CAME ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX, OPS CHECKED GOOD IAW MM 32-43-3. REMOVED AND REPLACED DUAL ANTI-SKID VALVE, OPS CHECKED GOOD IAW MM 27-60 AND 32-43. RESET G/B.
- [SDR ARWA980101](https://openairdocs.org/sdr/ARWA980101.md): Control Cable · broken · Jan 7, 1998 · N802BN · Doug DC862 · Rudder Control System
  > AIRCRAFT RETURNED TO BLOCKS RUDDER MOVEMENT LIMITED, HAS NOT FULL DEFLECTION WITH FLAPS DOWN. T/S FOUND RUDDER THROW LIMITER CABLE BROKEN. REMOVED AND REPLACED CABLE IAW 91-10-19 RIGGED IAW 27-50-0 OPS NORMAL.
- [SDR ARWA970901](https://openairdocs.org/sdr/ARWA970901.md): Duct · loose · Sep 7, 1997 · N802BN · Doug DC862 · Cabin Compressor System
  > UNABLE TO PRESSURISE ABOVE 1 PSI, 3 TC'S BLEEDS HIGH OUTFLOW HANDLE FULL UP AND LOCKED. DUMPED APPROXIMATELY 6.000 FUEL. FOUND EXHAUST DUCT OFF NR 3 T/C, REINSTALLED DUCT AND PRESSURIZED CABIN TO 4.5 PSI ON ENG RUN.
- [SDR ARWA9702002](https://openairdocs.org/sdr/ARWA9702002.md): Radar Scope · failed · Feb 6, 1997 · N802BN · Doug DC862 · Weather Radar System
  > AFTER DEPARTURE, WEATHER RADAR DID NOT PAINT TARGET. RETURNED TO MIAMI, TROUBLESHOT SYSTEM FOUND RADAR SCOPE FAILING. REMOVED AND REPLACED SCOPE, OPS CHECKED NORMAL.
- [SDR ARWA9611004](https://openairdocs.org/sdr/ARWA9611004.md): Compressor · malfunctioned · Nov 15, 1996 · N802BN · Doug DC862 · Cabin Compressor System
  > AIR TURNBACK, NR 4 TURBO COMPRESSOR OVERHEAT LIGHT ON. UNABLE TO HOLD CABIN ALTITUDE. RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 T/C, SYS OPS AND FUNCTIONAL TEST OK, IAW MM 21-2-1.
- [SDR ARWA9609030](https://openairdocs.org/sdr/ARWA9609030.md): Relay · malfunctioned · Sep 20, 1996 · N802BN · Doug DC862 · DC Power Distribution System
  > WHILE ON CLIMBOUT, LOST NR 1 DC BUS, CAPTAIN'S INSTRUMENTS LIGHTS OUT, 1 AND 2 ENGINE OIL TEMP, OIL QTY, CSD NR 1 FUEL FEED PUMP NR 1 ALT FUEL PUMP, HYD QTY. RETURNED TO MIAMI WITHOUT INCIDENT. WHEN PUT GEAR DOWN, ALL ABOVE RETURNED TO NORMAL. REMOVED AND R

Next page: https://openairdocs.org/deregistered/N802BN-2006-06-19/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 = 'N802BN' AND deregistration_id = 'N802BN-2006-06-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N802BN-2006-06-19/reports

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