# Service difficulty reports: N16808, cancelled Nov 13, 2002

A list on [N16808, cancelled Nov 13, 2002](https://openairdocs.org/deregistered/N16808-2002-11-13.md).

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

- [SDR CALA0100837](https://openairdocs.org/sdr/CALA0100837.md): Battery · discharged · Sep 7, 2001 · N16808 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND PORTABLE EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR INOPERATIVE. THE BATTERIES FOR THE PORTABLE EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0001957](https://openairdocs.org/sdr/CALA0001957.md): Skin · dented · Dec 19, 2000 · N16808 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT AFT FUSELAGE SKIN DENTED JUST AFT OF LOUVER. THE DENT WAS COLD WORKED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEETS 11 AND 20, AND 51-30-2.
- [SDR CALA0000113](https://openairdocs.org/sdr/CALA0000113.md): Skin · dented · Feb 1, 2000 · N16808 · Doug DC982 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SURFACE DENTED AT XFS 71 TO XFS 77.50. A DOUBLER WAS INSTALLED IAW EA9-5513-2-AD577 AND ECRA 5510-01482.
- [SDR CALA0000112](https://openairdocs.org/sdr/CALA0000112.md): Fitting · cracked · Feb 1, 2000 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN VERTICAL SUPPORT FITTING AT FS 200, LBL 50. THE VERTICAL SUPPORT FITTING WAS REPLACED IAW SRM 51-30-05.
- [SDR CALA0000111](https://openairdocs.org/sdr/CALA0000111.md): Skin · dented · Feb 1, 2000 · N16808 · Doug DC982 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND RT HORIZONTAL STABILIZER DENTED EIGHT FEET AND NINE FEET FROM STABILIZER ROOT AT LEADING EDGE. THE AREA WAS REPAIRED IAW SRM 55-03, PAGE 6 AND 6A. A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 125 FLIGHT HOURS AND TO INSTALL A PERMANENT REP
- [SDR CALA0000110](https://openairdocs.org/sdr/CALA0000110.md): Support · cracked · Feb 1, 2000 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LT WHEEL WELL FORWARD JAMB SUPPORT. AN ANGLE AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-11, 51-10-03, AND 53-10-01, FIGURE 2.
- [SDR CALA0000109](https://openairdocs.org/sdr/CALA0000109.md): Pan · gouged · Feb 1, 2000 · N16808 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND R-1 DOORJAMB LOWER PAN AT SILL PLATE GOUGED. THE R-1 DOOR JAMB LOWER PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 55.
- [SDR CALA0000080](https://openairdocs.org/sdr/CALA0000080.md): Seat Track · corroded · Jan 25, 2000 · N16808 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED BETWEEN STA 1040 AND 1338. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5.
- [SDR CALA0000055](https://openairdocs.org/sdr/CALA0000055.md): Web · cracked · Jan 21, 2000 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CRACKED AT FS 1174, LBL 43. THE CRACKED SECTION OF WEB WAS REMOVED AND A NEW SECTION AND DOUBLER WERE INSTALLED IAW SRM 51-30-5.
- [SDR CALA0000054](https://openairdocs.org/sdr/CALA0000054.md): Support · corroded · Jan 21, 2000 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT AT FS 200, BL 0 TO RBL 44 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9901547](https://openairdocs.org/sdr/CALA9901547.md): Battery Pack · discharged · Dec 2, 1999 · N16808 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND THE FIRST CLASS OVERHEAD EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE OVERHEAD LIGHTING CHECKED GOOD.
- [SDR CALA9800689](https://openairdocs.org/sdr/CALA9800689.md): Strut · required service · Apr 23, 1998 · N16808 · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF FROM ORD. THE CHECKLIST WAS PERFORMED AND WHEN THE GEAR WAS PUT DOWN IT EXTENDED WITH A BANG. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR STRUT FLAT. A FULL
- [SDR CALA9701765](https://openairdocs.org/sdr/CALA9701765.md): Cables · out of adjust · Dec 14, 1997 · N16808 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND THE AFT PASSENGER ENTRANCE DOOR HANDLE WAS EXCESSIVE. MAINTENANCE RIGGED THE TAILCONE IAW MM 53-53-00 AND OPERATION CHECKED GOOD. IN ADDITION, ONE LOCK LATCH PIN WAS REPLACED DUE TO WE
- [SDR CALA9701759](https://openairdocs.org/sdr/CALA9701759.md): Intercostal · cracked · Dec 11, 1997 · N16808 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 CRACK IN MAIN CABIN DOOR INTERCOSTAL. THE CRACK WAS IN RADIUS AND LOCATED AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9701758](https://openairdocs.org/sdr/CALA9701758.md): Jamb · corroded · Dec 11, 1997 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND DOOR JAMB BEAM OF MAIN BAGGAGE BIN CORRODED. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63 AND ECRA 5310-03642.
- [SDR CALA9701757](https://openairdocs.org/sdr/CALA9701757.md): Beam · cracked · Dec 10, 1997 · N16808 · Doug DC982 · Service Doors
  > INSPECTION FOUND A.75 CRACK IN FORWARD LOWER CORNER OF FORWARD SERVICE DOOR LOWER BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-02, 51-30-04, AND 51-30-05.
- [SDR CALA9700964](https://openairdocs.org/sdr/CALA9700964.md): Radio Panel · chafed wire · Jun 21, 1997 · N16808 · Doug DC982 · Audio Integrating System
  > THE OBSERVER'S RADIO PANEL STARTED TO SMOKE WHILE EN ROUTE. THE PANEL WAS REMOVED, THE CONNECTOR PLUGS WERE DISCONNECTED, AND THE SMOKE CEASED. THE FLIGHT CONTINUED TO MIA WHERE IT LANDED WITHOUT FURTHER PROBLEM. A CHAFED WIRE WAS FOUND BEHIND THE PANEL. T
- [SDR CALA9600966](https://openairdocs.org/sdr/CALA9600966.md): Ground Shift Rod · broken · Jul 5, 1996 · N16808 · Doug DC982 · Nose/Tail Landing Gear
  > THE AIR/GROUND SHIFT MECHANISM WOULD NOT COME OUT OF GROUND MODE AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND GROUND SHIFT ROD ON NOSE GEAR BROKEN. THE GROUND SHIFT ROD WAS REMOVED AND REPLACED.
- [SDR CAL960098](https://openairdocs.org/sdr/CAL960098.md): Skin · delaminated · Jan 21, 1996 · N16808 · Doug DC982 · Wing, Plate/Skin
  > MIA - INSPECTION FOUND RIGHT WING CENTER SPAR TRAILING EDGE LOWER PANEL BELOW INBOARD AND OUTBOARD ANTI-SKID VALVES DELAMINATED. THE DELAMINATED AREA WAS CUT OUT. A NEW CORE WAS INSTALLED AND FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-70-2. (M)
- [SDR CAL960094](https://openairdocs.org/sdr/CAL960094.md): Support · corroded · Jan 19, 1996 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND CORROSION ON FLOOR SUPPORT TRACK IN CENTER CARGO COMPARTMENT BETWEEN BS 570-695, LBL 20. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-1-0. (M)
- [SDR CAL960160](https://openairdocs.org/sdr/CAL960160.md): Bulkhead · cracked · Jan 17, 1996 · N16808 · Doug DC982 · Fuselage Main, Bulkhead
  > MIA - INSPECTION FOUND A.5 INCH CRACK IN CANTED BULKHEAD WEB JUST FORWARD OF RUDDER TRIM ACTUATOR DRUM AT FS 1490, RIGHT SIDE. THE CRACKED WEB WAS REMOVED AND A BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-02. (M)
- [SDR CAL960162](https://openairdocs.org/sdr/CAL960162.md): Angle · cracked · Jan 15, 1996 · N16808 · Doug DC982 · Vertical Stabilizer
  > MIA - INSPECTION FOUND A.5 INCH CRACK IN LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE EXTERNAL ATTACH ANGLES LOCATED BETWEEN BS 1401 TO 1429. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)
- [SDR CAL960159](https://openairdocs.org/sdr/CAL960159.md): Floor Web · cracked · Jan 15, 1996 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND AN 8 INCH CRACK IN SUB FLOOR WEB ON RIGHT SIDE, STATION 1300, STRINGER 18. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. (M)
- [SDR CAL960100](https://openairdocs.org/sdr/CAL960100.md): Skin · delaminated · Jan 15, 1996 · N16808 · Doug DC982 · Spoilers
  > MIA - INSPECTION FOUND RIGHT WING INBOARD SPOILER UPPER SKIN DELAMINATED AT FORWARD INBOARD AREA. THE DAMAGED CORE WAS CUT OUT AND A HOT BOND REPAIR WAS DONE IAW SRM 51-70-1A. (M)
- [SDR CAL960093](https://openairdocs.org/sdr/CAL960093.md): Support · corroded · Jan 15, 1996 · N16808 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND FLOOR BOARD SUPPORT HAT CHANNEL CORRODED IN MAIN CABIN AT STATION 1165. A NEW FLOOR BOARD SUPPORT HAT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-1. (M)
- [SDR CAL960095](https://openairdocs.org/sdr/CAL960095.md): Vane · gouged · Jan 14, 1996 · N16808 · Doug DC982 · Trailing Edge Flaps
  > MIA - INSPECTION FOUND TOP INBOARD END OF RIGHT WING 5TH FOREFLAP VANE HAD GOUGES. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-1-9A. (M)
- [SDR CAL960101](https://openairdocs.org/sdr/CAL960101.md): Vane · chafed · Jan 13, 1996 · N16808 · Doug DC982 · Trailing Edge Flaps
  > MIA - INSPECTION FOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE SEGMENT CHAFED WITH METAL CURLED AT INBOARD UPPER END. THE CHAFED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND HOT BONDED IAW SRM 51-1-40A. (M)
- [SDR CAL960099](https://openairdocs.org/sdr/CAL960099.md): Skin · chafed · Jan 13, 1996 · N16808 · Doug DC982 · Trailing Edge Flaps
  > MIA - INSPECTION FOUND LEFT WING INBOARD FLAP UPPER SURFACE CHAFED INTO TWENTY INCHES FROM OUTBOARD END. THE CHAFED AREA WAS CUT OUT. AN INTERNAL DOUBLER AND FILLER WERE FABRICATED IAW SRM 51-01, FIGURE 4 AND INSTALLED IAW SRM 51-30-0. (M)
- [SDR CAL960097](https://openairdocs.org/sdr/CAL960097.md): Skin · delaminated · Jan 13, 1996 · N16808 · Doug DC982 · Wing, Plate/Skin
  > MIA - INSPECTION FOUND LEFT WING LOWER TRAILING EDGE SKIN PANEL DELAMINATED AROUND MOUNT SCREWS FOR INBOARD AND OUTBOARD ANTI-SKID VALVES. THE PANEL WAS REPAIRED WITH FIBERGLASS OVERLAY IAW SRM 51-70-1. (M)
- [SDR CAL960096](https://openairdocs.org/sdr/CAL960096.md): Vane · dinged · Jan 13, 1996 · N16808 · Doug DC982 · Trailing Edge Flaps
  > MIA - INSPECTION FOUND LOWER SURFACE OF INBOARD LEFT FLAP VANE DINGED AND ERODED DUE TO IMPACT DAMAGE CAUSED BY TIRE DEBRIS. A HOT BOND REPAIR WAS PERFORMED IAW SRM 51-1-9A. (M)
- [SDR CAL960106](https://openairdocs.org/sdr/CAL960106.md): Battery Pack · discharged · Jan 11, 1996 · N16808 · Doug DC982 · Emergency Lighting
  > MIA - INSPECTION FOUND THE FORWARD ENTRY EMERGENCY LIGHT DIM. THE BATTERIES FOR THE EMERGENCY LIGHT WERE REMOVED, RECHARGED, AND REINSTALLED. (M)
- [SDR CAL960105](https://openairdocs.org/sdr/CAL960105.md): Battery Pack · discharged · Jan 11, 1996 · N16808 · Doug DC982 · Emergency Lighting
  > MIA - INSPECTION FOUND THE AISLE OVERHEAD EMERGENCY LIGHT AT AFT GALLEY TO LAV INOPERATIVE. THE BATTERIES FOR THE EMERGENCY LIGHT WERE REMOVED, CHARGED, AND REINSTALLED. (M)
- [SDR CAL960103](https://openairdocs.org/sdr/CAL960103.md): Battery · discharged · Jan 11, 1996 · N16808 · Doug DC982 · Emergency Lighting
  > MIA - INSPECTION FOUND AFT GALLEY EMEREGNCY LIGHT DIM. THE BATTERIES FOR THE LIGHT WERE REMOVED, CHARGED AND REINSTALLED. (M)
- [SDR CAL960102](https://openairdocs.org/sdr/CAL960102.md): Battery Pack · discharged · Jan 11, 1996 · N16808 · Doug DC982 · Emergency Lighting
  > MIA - INSPECTION FOUND FORWARD GALLEY EMERGENCY LIGHT DIM. THE BATTERY PACK WAS REPLACED AND A LAMP WAS INSTALLED PER MM 33-50-0. (M)
- [SDR CAL951181](https://openairdocs.org/sdr/CAL951181.md): Clamp · broken · Dec 28, 1995 · N16808 · Doug DC982 · Pneumatic Distribution System
  > FLT 1263 - CLE - THE NR 2 ENG FIRE WARN LIGHT ILLUMINATED DURING CLIMB-OUT OF CLE. THE FIRE LIGHT WENT OUT FOR ABOUT 1 MIN AFTER LEVELING OFF, AND CAME ON AGAIN FOR ABOUT 15 SEC. THE FIRE WARN WAS ACCOMPANIED BY NR 2 ENG OIL QTY LOSS AND THE CABIN WOULD NOT
- [SDR CAL950596](https://openairdocs.org/sdr/CAL950596.md): Gen Contl Pnl · inoperative · Jul 15, 1995 · N16808 · Doug DC982 · AC Generation System
  > GSO - FLT 0402 - THE RIGHT CSD OIL TEMP WENT OFF SCALE HIGH AFTER TAKEOFF FROM MCO. THE CSD WAS DISCONNECTED AND THE APU WAS STARTED TO POWER THE RIGHT AC BUS. THE APU GENERATOR FREQUENCY STARTED FLUCTUATING FULL SCALE DEFLECTION BOTH WAYS. THE APU GENERATO

## 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 = 'N16808' AND deregistration_id = 'N16808-2002-11-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16808-2002-11-13/reports

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