# Service difficulty reports: N18835, cancelled Jun 23, 2005

A list on [N18835, cancelled Jun 23, 2005](https://openairdocs.org/deregistered/N18835-2005-06-23.md).

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

- [SDR CALA0400616](https://openairdocs.org/sdr/CALA0400616.md): Flange · cracked · Aug 25, 2004 · N18835 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3 INCH CRACK IN THE AFT CARGO DOOR FORWARD LOWER STOP FLANGE. REPAIRED IAW ECRA 5232-01047.
- [SDR CALA0400609](https://openairdocs.org/sdr/CALA0400609.md): Release Cable · out of rig · Aug 20, 2004 · N18835 · Doug DC982 · Aerodynamic Fairings
  > THE TAILCONE PULL CHECK FROM THE INTERIOR RELEASE HANDLE, FAILED. THE CABLES WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA0400602](https://openairdocs.org/sdr/CALA0400602.md): Seat Track · corroded · Aug 13, 2004 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1007-1098, BL 0 TO LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA0400601](https://openairdocs.org/sdr/CALA0400601.md): Skin · cracked · Aug 13, 2004 · N18835 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, BETWEEN LONGERON 13R AND 14R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 18.
- [SDR CALA0400600](https://openairdocs.org/sdr/CALA0400600.md): Skin · cracked · Aug 13, 2004 · N18835 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, LONGERON 13L TO 14L. THE CRACKED AREA OF SKIN WAS CUT OUT AND FILLER AND A DOUBLER WERE INSTALLED IAW SRM 53-04, FIGURE 18 AND 51-10-3B.
- [SDR CALA0400598](https://openairdocs.org/sdr/CALA0400598.md): Seat Track · corroded · Aug 12, 2004 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 200-218, RBL 22. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05.
- [SDR CALA0400596](https://openairdocs.org/sdr/CALA0400596.md): Seat Track · corroded · Aug 12, 2004 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT MID SEAT TRACK CORRODED FROM STA 1098-1201, LBL 30. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0400593](https://openairdocs.org/sdr/CALA0400593.md): Floor Support · corroded · Aug 6, 2004 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1155 BETWEEN LT IB AND LT MID SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-5.
- [SDR CALA0300654](https://openairdocs.org/sdr/CALA0300654.md): Skin · corroded · Nov 20, 2003 · N18835 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LOWER T/E SKIN CORRODED AT REAR SPAR STA XRS 399-477. A SKIN DOUBLER WAS INSTALLED IAW ECRA 5731-01037.
- [SDR CALA0300653](https://openairdocs.org/sdr/CALA0300653.md): Spar · corroded · Nov 20, 2003 · N18835 · Doug DC982 · Wing Spar
  > INSPECTION FOUND RT WING FORWARD SPAR CORRODED AT STA XRS 258-335. REPAIRED IAW ECRA 5731-01040.
- [SDR CALA0200467](https://openairdocs.org/sdr/CALA0200467.md): Web · corroded · Sep 18, 2002 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN SUB FLOOR STRUCTURE PLATE(WEB) CORRODED BETWEEN STA 1211 AND 1231 ABOVE LONGERON 28L-27R. REPAIRED IAW ECRA 5311-01133.
- [SDR CALA0200205](https://openairdocs.org/sdr/CALA0200205.md): Charger · failed · Apr 15, 2002 · N18835 · Doug DC982 · Emergency Lighting
  > THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 5-12 WERE FOUND INOPERATIVE DURING S CHECK INSPECTION. TROUBLESHOOTING IAW WDM 33-51-14 FOUND THE BATTERY CHARGER AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA0001161](https://openairdocs.org/sdr/CALA0001161.md): Spacer · worn · Jul 27, 2000 · N18835 · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > THE NLG GEAR WOULD NOT FULLY RETRACT DURING TEST FLIGHT. MAINTENANCE FOUND THE NLG UPPER BEARING STRUT SPACER AND RING DAMAGED/WORN. THE NLG STRUT WAS REMOVED. THE SPACER AND NOSE STRUT SEALS WERE REPLACED IAW MM 32-21-02, PARAGRAPH 3A AND 3B. THE NLG STRU
- [SDR CALA0001147](https://openairdocs.org/sdr/CALA0001147.md): Pan · cracked · Jul 24, 2000 · N18835 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN SECOND FROM THE TOP MID CARGO DOOR AFT STOP PAD. A DOUBLER WAS INSTALLED ON DOOR PAN IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01565.
- [SDR CALA0001120](https://openairdocs.org/sdr/CALA0001120.md): Skin · damaged · Jul 21, 2000 · N18835 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERIOR FUSELAGE SKIN CREASED AT STA 256, LONGERON 18L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02978.
- [SDR CALA0001119](https://openairdocs.org/sdr/CALA0001119.md): Cable · frayed · Jul 21, 2000 · N18835 · Doug DC982 · Aerodynamic Fairings
  > INSPECTION FOUND UPPER LEFT O/B AREA OF TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REPLACED AND TAIL CONE RELEASE MECHANISM WAS RIGGED IAW MM 53-53-00.
- [SDR CALA0001086](https://openairdocs.org/sdr/CALA0001086.md): Pan · worn · Jul 17, 2000 · N18835 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR AFT SIDE NR 1 STOP PAD AND FORWARD SIDE NR 5 STOP PAD WORN. REPAIRED IAW ECRA 5230-01540.
- [SDR CALA0001085](https://openairdocs.org/sdr/CALA0001085.md): Door Frame · corroded · Jul 17, 2000 · N18835 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB CORRODED. REPAIRED IAW SRM 53-05, FIGURE 44.
- [SDR CALA0001082](https://openairdocs.org/sdr/CALA0001082.md): Spacer · corroded · Jul 17, 2000 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR Z-BEAM SPACER CORRODED AT STA 1155 - 1212. THE LOWER DOOR Z-BEAM SPACER WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0001092](https://openairdocs.org/sdr/CALA0001092.md): Skin · dented · Jul 14, 2000 · N18835 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 BELOW LONGERON 16L AFT OF MAIN CABIN DOOR. THE DENT WAS COLD WORKED AND A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.
- [SDR CALA0001067](https://openairdocs.org/sdr/CALA0001067.md): Skin · dented · Jul 14, 2000 · N18835 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERIOR SKIN DENTED AT STA 237, LONGERON 17L TO 18L. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-02445.
- [SDR CALA0001060](https://openairdocs.org/sdr/CALA0001060.md): Longeron · bent · Jul 12, 2000 · N18835 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 16R BENT FROM STA 250 - 252. A LONGERON SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18.
- [SDR CALA0001031](https://openairdocs.org/sdr/CALA0001031.md): Seat Track · corroded · Jul 11, 2000 · N18835 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 200 - 245. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, SHEETS 1, 9 AND 10.
- [SDR CALA9900819](https://openairdocs.org/sdr/CALA9900819.md): Battery Charger · inoperative · Jul 13, 1999 · N18835 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND TAIL CONE EMERGENCY AISLE PATH LIGHTING INOPERATIVE. THE BATTERY CHARGER AT AFT SERVICE DOOR OVERHEAD PANEL WAS REMOVED AND REPLACED IAW MM 33-50.
- [SDR CALA9801156](https://openairdocs.org/sdr/CALA9801156.md): Clips · out of adjust · Jun 23, 1998 · N18835 · Doug DC982 · Aerodynamic Fairings
  > THE TAIL CONE RELEASE HANDLE INSIDE TAIL COMPARTMENT PULLED HIGH FROM CLIPS AT 45 POUNDS. THE CLIPS WERE ADJUSTED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-50-00.
- [SDR CALA9801155](https://openairdocs.org/sdr/CALA9801155.md): Cables · out of adjust · Jun 22, 1998 · N18835 · Doug DC982 · Aerodynamic Fairings
  > THE TAIL CONE PULL FROM INTERIOR RELEASE HANDLE, EXTERIOR RELEASE HANDLE, AND AFT ENTRY DOOR WAS LOW. THE TAIL CONE CABLES WERE RIGGED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-53-00.
- [SDR CALA9801154](https://openairdocs.org/sdr/CALA9801154.md): Rail · corroded · Jun 22, 1998 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT TIE DOWN RAIL HAD EXFOLIATED CORROSION AT ATTACH FASTENER AND BELTFRAME AT STA 1022 WITH LIGHT TO MODERATE CORROSION AT STA 1003 TO 1221. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801145](https://openairdocs.org/sdr/CALA9801145.md): Pivot Plates · corroded · Jun 19, 1998 · N18835 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND VERTICAL FIN RIGHT SIDE INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED IN SLEEVE BORE. THE INBOARD AND OUTBOARD SET OF PIVOT PLATES WERE REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA9801132](https://openairdocs.org/sdr/CALA9801132.md): Skin · dented · Jun 19, 1998 · N18835 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A DENT IN RT FUSELAGE SKIN AT STA 282. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA9801128](https://openairdocs.org/sdr/CALA9801128.md): Jamb · corroded · Jun 19, 1998 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO COMPARTMENT DOOR JAMB Z-ANGLE BEAM CORRODED AT STA 1155-1211, LONGERON 26R. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA9801127](https://openairdocs.org/sdr/CALA9801127.md): Intercostal · cracked · Jun 18, 1998 · N18835 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND THE MAIN CABIN DOOR INTERCOSTAL JUST AFT OF LOCK MECHANISM HAD A 1/2 CRACK AT EXTERNAL HANDLE RECESS. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9801126](https://openairdocs.org/sdr/CALA9801126.md): Beam · cracked · Jun 17, 1998 · N18835 · Doug DC982 · Service Doors
  > INSPECTION FOUND A 1.5 CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA9801123](https://openairdocs.org/sdr/CALA9801123.md): Beam · cracked · Jun 17, 1998 · N18835 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1/2 CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW SRM 51-30, 51-30-2, 51-30-5.
- [SDR CALA9800844](https://openairdocs.org/sdr/CALA9800844.md): Slide · failed · May 12, 1998 · N18835 · Doug DC982 · Escape Slide
  > TAIL CONE DEPARTED AIRCRAFT AND SLIDE FAILED TO COMPLETELY DEPLOY. REPLACED SLIDE AND TAIL CONE ASSEMBLY PER MM 25-63-01 AND 53-53-00.
- [SDR CALA9800399](https://openairdocs.org/sdr/CALA9800399.md): Bolt · loose · Mar 8, 1998 · N18835 · Doug DC982 · Landing Gear Position and Warning
  > THE GROUND SHIFT SWITCH FAILED TO MOVE TO THE FLIGHT MODE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT RAISE. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOLT BACKED OUT OF NOSE GEAR OLEO SWITCH. REPLACED HARDWARE IAW I
- [SDR CALA9700491](https://openairdocs.org/sdr/CALA9700491.md): Control Valve · leaking · Apr 6, 1997 · N18835 · Doug DC982 · Landing Gear Retraction/Extension System
  > THE RIGHT HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ON APPROACH TO EWR, THE LANDING GEAR WAS EXTENDED MANUALLY. THE AIRCRAFT LANDED AT EWR WITH DAMAGE TO THE RT MLG DOOR AND SKID PLATE. MAINTENANCE FOUND THE LANDING GEAR CONTROL VALVE LEAKING. NEW PACKING WA
- [SDR CALA9601139](https://openairdocs.org/sdr/CALA9601139.md): Circuit Breaker · tripped · Aug 8, 1996 · N18835 · Doug DC982 · AC Generation System
  > WHILE OPERATING THE APU ON TAKEOFF WITH THE LT GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR WAS LOST AND HAD NO CROSSTIE. THE APU GENERATOR COULD NOT BE RESET AND THE AIRCRAFT WAS RETURNED TO LAS. MAINTENANCE FOUND THE APU CONTROL CIRCUIT BREAKER POPPE
- [SDR CALA9600955](https://openairdocs.org/sdr/CALA9600955.md): Latches · out of adjust · Jun 29, 1996 · N18835 · Doug DC982 · Aerodynamic Fairings
  > THE PULL REQUIRED TO RELEASE TAILCONE USING THE EXTERIOR HANDLE WAS LOW. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-10.
- [SDR CALA9600954](https://openairdocs.org/sdr/CALA9600954.md): Clips · out of adjust · Jun 29, 1996 · N18835 · Doug DC982 · Aerodynamic Fairings
  > EXCESSIVE PULL WAS REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA9600958](https://openairdocs.org/sdr/CALA9600958.md): Floor Support · corroded · Jun 19, 1996 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON FLOOR SUPPORT INBOARD OF FORWARD ENTRY DOOR AT STA 180 TO 195. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9600957](https://openairdocs.org/sdr/CALA9600957.md): Floor Support · corroded · Jun 19, 1996 · N18835 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT AT AFT SERVICE DOOR CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5 AND 51-10-3.
- [SDR CAL950637](https://openairdocs.org/sdr/CAL950637.md): Postion Sensor · out of adjust · Aug 3, 1995 · N18835 · Doug DC982 · Landing Gear Position and Warning
  > IAH - FLT 0664 - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. MAINTENANCE FOUND THE NOSE GEAR UP/DOWN POSITION SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED PER MM 32-60-05 AND OPERATION CHECKED GOOD.
- [SDR CAL950603](https://openairdocs.org/sdr/CAL950603.md): Switch · inoperative · Jul 18, 1995 · N18835 · Doug DC982 · Landing Gear Position and Warning
  > FLT NR 0117 - LAX - ALL THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WHILE IN FLIGHT. THE GEAR WAS CYCLED, BUT THE LIGHTS DID NOT EXTINGUISH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE S1-319 LEFT THROTTLE SWITCH IN THE PEDESTAL AT FAULT. THE
- [SDR CAL950214](https://openairdocs.org/sdr/CAL950214.md): Hyd Line · ruptured · Mar 18, 1995 · N18835 · Doug DC982 · Hydraulic System, Main
  > IAH - FLT 0459 - LT HYDRAULIC SYSTEM PRESSURE AND QUANTITY BEGAN TO DECREASE IN-FLIGHT. THE LT ENGINE HYDRAULIC PUMP WAS TURNED OFF AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE FROM LT PYLON FITTING TO ENGINE CASE DRA
- [SDR CAL950048](https://openairdocs.org/sdr/CAL950048.md): Clip · broken · Jan 11, 1995 · N18835 · Doug DC982 · Aerodynamic Fairings
  > HOU - THE FORCE REQUIRED TO PULL HANDLE FROM CLIPS WAS TOO LOW DURING TAIL CONE DROP TEST. REMOVED AND REPLACED BROKEN CLIP. (W)
- [SDR CAL950047](https://openairdocs.org/sdr/CAL950047.md): Cables · out of adjust · Jan 11, 1995 · N18835 · Doug DC982 · Aerodynamic Fairings
  > HOU - THE TAILCONE RELEASE PULL TEST FAILED AT ALL THREE POSITIONS. THE TAILCONE RELEASE CABLES WERE RIGGED PER MM 53-53-00, PARAGRAPH 3A, PAGE 502, CONFIGURATION 1. (Z)

## 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 = 'N18835' AND deregistration_id = 'N18835-2005-06-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N18835-2005-06-23/reports

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