# Service difficulty reports: N16887, cancelled May 22, 2003

A list on [N16887, cancelled May 22, 2003](https://openairdocs.org/deregistered/N16887-2003-05-22.md).

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

- [SDR CALA0100538](https://openairdocs.org/sdr/CALA0100538.md): Battery · discharged · Jun 12, 2001 · N16887 · Doug DC982 · Emergency Equipment
  > INSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA0001374](https://openairdocs.org/sdr/CALA0001374.md): Battery Pack · inoperative · Sep 3, 2000 · N16887 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0001293](https://openairdocs.org/sdr/CALA0001293.md): Angle · corroded · Aug 21, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-ANGLE CORRODED UNDER EXISTING DOUBLER AT CANTED BULKHEAD STA 1463, L16R. A NEW ANGLE SECTION WAS INSTALLED IAW SRM 53-03, FIGURE 27.
- [SDR ALA0001292](https://openairdocs.org/sdr/ALA0001292.md): Floorbeam · corroded · Aug 21, 2000 · N16887 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATE MOUNT AREA, STA 1338 BELOW LT AFT LAV. A SPLICE SECTION WAS INSTALLED IAW SRM 51-30-0 AND 51-10-3.
- [SDR CALA0001274](https://openairdocs.org/sdr/CALA0001274.md): Attach Angle · cracked · Aug 18, 2000 · N16887 · Doug DC982 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1486, L3R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23.
- [SDR CALA0001271](https://openairdocs.org/sdr/CALA0001271.md): Skin · dented · Aug 16, 2000 · N16887 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17L AND 18L. THE SKIN SECTION WAS REPLACED IAW ECRA 5330-02445.
- [SDR CALA0001270](https://openairdocs.org/sdr/CALA0001270.md): Web · cracked · Aug 16, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN WEB AT CANTED BULKHEAD STA 1463, LONGERON 17R. THE CRACKED SECTION OF WEB WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, SHEET 3.
- [SDR CALA0001269](https://openairdocs.org/sdr/CALA0001269.md): Pan · chafed · Aug 16, 2000 · N16887 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MAIN BAGGAGE BIN DOOR PAN CHAFED AT FORWARD EDGE OF NR 1 STOP PAD. REPAIRED IAW ECRA 5230-01540.
- [SDR CALA0001268](https://openairdocs.org/sdr/CALA0001268.md): Pan · cracked · Aug 16, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.25 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN UNDER NR 4 STOP PAD BRACKET AT AFT EDGE OF DOOR. REPAIRED IAW SRM 52-05, FIGURE 26A AND 50.
- [SDR CALA0001267](https://openairdocs.org/sdr/CALA0001267.md): Floorbeam · worn · Aug 15, 2000 · N16887 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM WORN AT RT CENTER OF FORWARD CARGO BEAM, STA 389. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 86.
- [SDR CALA0001265](https://openairdocs.org/sdr/CALA0001265.md): Skin · dented · Aug 14, 2000 · N16887 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF THE L-1 DOOR AND APPROXIMATELY 8 INCHES ABOVE FORWARD LAV SERVICE PANEL AT STA 226, LONGERON 17L-18L. INSPECTION FOUND THE DENT TO BE IN CONDITION (1) PER SRM 53-04, PAGE 218, TABLE C. THE DENT WAS BLENDED OUT AND
- [SDR CALA0001264](https://openairdocs.org/sdr/CALA0001264.md): Fitting · corroded · Aug 14, 2000 · N16887 · Doug DC982 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND LT SIDEWALL LOWER ATTACH FITTING CORRODED AT STA 200. A NEW FITTING WAS INSTALLED IAW SRM 51-30.
- [SDR CALA0001245](https://openairdocs.org/sdr/CALA0001245.md): Angle · corroded · Aug 8, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN BAGGAGE BIN DOOR JAMB Z-ANGLE CORRODED AT I/B SIDE AROUND HI-SHEARS. THE CORROSION ON DOOR FRAME Z-ANGLE WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA0001244](https://openairdocs.org/sdr/CALA0001244.md): Web · corroded · Aug 8, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CUSP MEMBRANE CORRODED AT STA 200 JUST AFT OF MCD CUTOUT AT LOWER SIDE. THE CUSP MEMBRANE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND ECRA 5310-03778.
- [SDR CALA0001232](https://openairdocs.org/sdr/CALA0001232.md): Seat Track · corroded · Aug 4, 2000 · N16887 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 236. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA9901511](https://openairdocs.org/sdr/CALA9901511.md): Battery Pack · discharged · Nov 18, 1999 · N16887 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS ABOVE BOTH LEFT AND RIGHT DOORS INOPERATIVE DURING EMERGENCY LIGHT TEST. THE POWER SUPPLY BATTERY PACK WAS REMOVED AND REPLACED. OPERATION CHECKED GOOD IAW MM 33-53-00, PAGE 407.
- [SDR CALA9900214](https://openairdocs.org/sdr/CALA9900214.md): Strut · reqd service · Mar 5, 1999 · N16887 · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > THE LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE NLG STRUT FLAT. A COMPLETE STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. THE NOSE GEAR WAS CYCLED AND LANDING GEAR
- [SDR CALA9801212](https://openairdocs.org/sdr/CALA9801212.md): Pins · worn · Jul 6, 1998 · N16887 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO RELEASE TAILCONE USING EXTERIOR HANDLE WAS BELOW LIMITS. WORN ALIGNMENT PINS AND RECEPTACLES WERE REPLACED AND LATCHES WERE ADJUSTED IAW MM 53-50-00.
- [SDR CALA9801211](https://openairdocs.org/sdr/CALA9801211.md): Web · corroded · Jul 2, 1998 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED AT STA 1212 AFT OF DOOR INBOARD OF LONGERON 27R. A REPAIR WAS INSTALLED IAW ECRA 5310-03742.
- [SDR CALA9801186](https://openairdocs.org/sdr/CALA9801186.md): Skin · cracked · Jun 30, 1998 · N16887 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.25 INCH CRACK IN MAIN CABIN DOOR SKIN WITH DEEP WEAR MARKS ON HOLD OPEN HOOK PAN ON DOOR. A REPAIR DOUBLER WAS INSTALLED AND THE PAN WAS REPLACED IAW SRM 52-05.
- [SDR CALA9801185](https://openairdocs.org/sdr/CALA9801185.md): Spacer · corroded · Jun 29, 1998 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON AFT BAGGAGE BIN Z-ANGLE REPAIR SPACER AT STA 1155 TO 1212. THE REPAIR SPACER WAS REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA9801184](https://openairdocs.org/sdr/CALA9801184.md): Intercostal · cracked · Jun 29, 1998 · N16887 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.5 INCH CRACK AT EXTERNAL HANDLE RECESS CUP OF MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801182](https://openairdocs.org/sdr/CALA9801182.md): Beam · cracked · Jun 26, 1998 · N16887 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.25 INCH CRACK IN RADIUS OF MAIN CABIN DOOR NR 1 HORIZONTAL BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31.
- [SDR CALA9801176](https://openairdocs.org/sdr/CALA9801176.md): Beam · cracked · Jun 26, 1998 · N16887 · Doug DC982 · Galley Doors
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FORWARD GALLEY SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9601340](https://openairdocs.org/sdr/CALA9601340.md): Fuel Control · leaking · Sep 29, 1996 · N16887 · Doug DC982 · APU Engine Fuel and Control
  > A STRONG FUEL SMELL WAS NOTICED IN THE COCKPIT AND CABIN WHILE DESCENDING INTO CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LEAKING FROM APU FUEL CONTROL DRAIN. THE APU FUEL CONTROL UNIT WAS REMOVED AND REPLACED PER MM 49-01-1. THE APU
- [SDR CALA9601102](https://openairdocs.org/sdr/CALA9601102.md): Clips · out of adjust · Jul 25, 1996 · N16887 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO PULL INTERIOR AND EXTERIOR TAILCONE RELEASE HANDLES OUT OF CLIPS WAS EXCESSIVE. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA9601094](https://openairdocs.org/sdr/CALA9601094.md): Hat Section · corroded · Jul 17, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND HAT SECTION CORRODED AROUND NUTPLATE HOLE BETWEEN PANEL J AND H AT FORWARD ENTRY. THE HAT SECTION WAS REMOVED AND A NEW HAT SECTION WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA9601097](https://openairdocs.org/sdr/CALA9601097.md): Sub Floor · corroded · Jul 12, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND BOTTOM OF SUB-FLOOR CORRODED OUTBOARD OF LEFT OUTBOARD SEAT TRACK AT STA 1136-1274. THE SUB-FLOOR WAS REPLACED IAW SRM 51-30-02.
- [SDR CALA9601099](https://openairdocs.org/sdr/CALA9601099.md): Channel · cracked · Jul 11, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-CHANNEL CRACKED AT STA 69. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, PAGE 9 AND SRM 51-30-5.
- [SDR CALA9601095](https://openairdocs.org/sdr/CALA9601095.md): Intercostal · cracked · Jul 11, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FIVE 1 INCH CRACKS IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 1309. THE CRACKS WERE STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2.
- [SDR CALA9601096](https://openairdocs.org/sdr/CALA9601096.md): Intercostal · cracked · Jul 10, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 10 INCH CRACK IN FORWARD BAGGAGE BIN INTERCOSTAL AT VHF ANTENNA MOUNT BETWEEN STA 465 AND STA 484. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9601101](https://openairdocs.org/sdr/CALA9601101.md): Latches · out of adjust · Jul 9, 1996 · N16887 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND AFT ENTRANCE DOOR RELEASE HANDLE WAS EXCESSIVE. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA9601100](https://openairdocs.org/sdr/CALA9601100.md): Skin · dented · Jul 8, 1996 · N16887 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF PITOT TUBES. THE DENTED SECTION OF SKIN WAS REPLACED IAW SRM 51-30-2 AND SRM 51-30-5.
- [SDR CALA9601098](https://openairdocs.org/sdr/CALA9601098.md): Skin · dented · Jul 8, 1996 · N16887 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN LONGERON 21R AND 22R AT STA 165. THE DENT WAS COLD-FORMED AND DYE CHECKED WITH NO CRACKS FOUND. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, PAGE 218.
- [SDR CALA9600770](https://openairdocs.org/sdr/CALA9600770.md): Hyd Line · leaking · Jun 8, 1996 · N16887 · Doug DC982 · Hydraulic System, Main
  > THE RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHILE EN ROUTE. EMERGENCY GEAR EXTENSION WAS USED PRIOR TO LANDING. THE LT MLG DOOR WAS DAMAGED UPON LANDING AT EWR. MAINTENANCE FOUND THE HYDRAULIC LINE FOR NOSE GEAR UP LEAKING AND THE LINE
- [SDR CAL960542](https://openairdocs.org/sdr/CAL960542.md): Oil Tank Vent · clogged · Apr 27, 1996 · N16887 · Doug DC982 · APU Oil System
  > FLT NR 279 - EWR - PRIOR TO PUSH BACK CABIN BEGAN TO FILL WITH SMOKE. DURING T/S FOUND OIL LEAKED ON COALESCER BAGS DUE TO APU OIL TANK BEING OVERSERVICED. REMOVED AND REPLACED COALESCER BAGS CLEANED APU OIL TANK VENT HOLE, DRAINED 2 QTS OF OIL. TANK NOW RE

## 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 = 'N16887' AND deregistration_id = 'N16887-2003-05-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16887-2003-05-22/reports

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