# Service difficulty reports: N35836, cancelled Jun 29, 2005

A list on [N35836, cancelled Jun 29, 2005](https://openairdocs.org/deregistered/N35836-2005-06-29.md).

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

- [SDR CALA0500042](https://openairdocs.org/sdr/CALA0500042.md): Seat Track · corroded · Feb 6, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND F/O'S AFT O/B SEAT TRACK CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-40-01.
- [SDR CALA0500041](https://openairdocs.org/sdr/CALA0500041.md): Panel · cracked · Feb 3, 2005 · N35836 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN UPPER TRAILING EDGE PANEL LOCATED FORWARD OF O/B SIDE OF GROUND SPOILER, LEFT UPPER WING, XRS 91.0 TO 111.5. A NEW PANEL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0500040](https://openairdocs.org/sdr/CALA0500040.md): Door Frame · cracked · Feb 3, 2005 · N35836 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND A 1.75 INCH CRACK IN NWW LT DOOR JAMB AT UPPER LOCK FASTENER FOR SPRAY DEFLECTOR GUARD, STA 45. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 110.
- [SDR CALA0500036](https://openairdocs.org/sdr/CALA0500036.md): Skin · cracked · Feb 1, 2005 · N35836 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK BELOW LOWER FORWARD LATCH OF MID CARGO DOOR SKIN. THE DOOR SKIN WAS REPAIRED IAW SRM 52-05, FIGURE 26A.
- [SDR CALA0500035](https://openairdocs.org/sdr/CALA0500035.md): Pan · cracked · Jan 31, 2005 · N35836 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A.75 INCH CRACK AT CORNER OF LOWER FORWARD INNER PAN OF FORWARD CARGO DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A.
- [SDR CALA0500031](https://openairdocs.org/sdr/CALA0500031.md): Floor Panel · delaminated · Jan 29, 2005 · N35836 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND LT CENTER FLOOR PANEL DELAMINATED AND HOLES PUNCHED IN PANEL AT STA 465-541, LBL 20 TO LBL 40. A NEW PANEL WAS INSTALLED IAW SRM 53-05, PAGE 122B.
- [SDR CALA0500028](https://openairdocs.org/sdr/CALA0500028.md): Floorbeam · corroded · Jan 28, 2005 · N35836 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1322 UNDER RT LAV, RBL 20. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 79A.
- [SDR CALA0500025](https://openairdocs.org/sdr/CALA0500025.md): Floor Support · cracked · Jan 27, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK AT FORWARD O/B END OF FORWARD ENTRY FLOOR SUPPORT TEE AT STA 180, RBL 43. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.
- [SDR CALA0500024](https://openairdocs.org/sdr/CALA0500024.md): Seat Track · corroded · Jan 26, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT MIDDLE SEAT TRACK CORRODED FROM STA 1022-1250, S18L. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA0500022](https://openairdocs.org/sdr/CALA0500022.md): Structure · corroded · Jan 26, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUBFLOOR CORRODED UNDER LEFT O/B SEAT TRACK AT STA 1174, LBL 60. THE CORRODED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-70-4.
- [SDR CALA0500021](https://openairdocs.org/sdr/CALA0500021.md): Seat Track · corroded · Jan 24, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1022-1250, LBL 25. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4.
- [SDR CALA0500020](https://openairdocs.org/sdr/CALA0500020.md): Seat Track · corroded · Jan 22, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CAPTAIN'S AFT I/B SEAT TRACK CORRODED AT STA 83.55 - 101.55, LBL 10. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01.
- [SDR CALA0500017](https://openairdocs.org/sdr/CALA0500017.md): Floorbeam · corroded · Jan 21, 2005 · N35836 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 180, LBL 12 TO LBL 37. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2.
- [SDR CALA0500016](https://openairdocs.org/sdr/CALA0500016.md): Rib · cracked · Jan 21, 2005 · N35836 · Doug DC982 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A.75 INCH CRACK IN RIB AND DOUBLER AT LT WING LEADING EDGE INTERNALLY BETWEEN NR 9 AND NR 10 SLAT TRACK CUTOUTS, STA XRS 324. THE CRACKED RIB AND CLIP ANGLE WERE REMOVED AND A NEW RIB AND CLIP ANGLE WERE INSTALLED IAW SRM 51-10-03, 51-30-02,
- [SDR CALA0500057](https://openairdocs.org/sdr/CALA0500057.md): Cusp Web · corroded · Jan 20, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT CUSP CORRODED AT STA 200. A SMALL SECTION OF THE UPPER CUSP CHORD WAS TRIMMED OUT TO REMOVE LOCAL CORROSION AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5311-01216.
- [SDR CALA0500012](https://openairdocs.org/sdr/CALA0500012.md): Longeron · cracked · Jan 17, 2005 · N35836 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.75 INCH CRACK IN LONGERON 4L AT STA 160. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02 FIGURE 18.
- [SDR CALA0500009](https://openairdocs.org/sdr/CALA0500009.md): Floor Support · corroded · Jan 16, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CENTER FLOOR SUPPORT BETWEEN I/B AND MIDDLE SEAT TRACKS CORRODED AROUND SCREW HOLES AT LT SIDE STA 1155, BL 0 TO LBL 30. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-01.
- [SDR CALA0100894](https://openairdocs.org/sdr/CALA0100894.md): Clip · out of adj · Sep 23, 2001 · N35836 · Doug DC982 · Aerodynamic Fairings
  > THE TAILCONE EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA0100893](https://openairdocs.org/sdr/CALA0100893.md): Frame · cracked · Sep 21, 2001 · N35836 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L3R AN L26L. THE CRACKED FRAME CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0100891](https://openairdocs.org/sdr/CALA0100891.md): Fitting · cracked · Sep 20, 2001 · N35836 · Doug DC982 · Spoilers
  > INSPECTION FOUND A 2.5" CRACK IN R/H WING GROUND SPOILER ACTUATOR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5740-01317 AND DRAWING SRO9570010.
- [SDR CALA0100890](https://openairdocs.org/sdr/CALA0100890.md): Fitting · cracked · Sep 20, 2001 · N35836 · Doug DC982 · Spoilers
  > INSPECTION FOUND A 2.25" CRACK IN L/H WING LEFT I/B GROUND SPOILER ACTUATOR SUPPORT FITTING. REPAIRED IAW ECRA 5740-01317 AND DRAWING SR09570010.
- [SDR CALA0100887](https://openairdocs.org/sdr/CALA0100887.md): Door Frame · corroded · Sep 19, 2001 · N35836 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND MID BAGGAGE BIN LOWER DOOR JAMB CORRODED AROUND H-SHEAR AT STA 636-693. A REPAIR DOUBLER AND SPACER WERE INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA0100886](https://openairdocs.org/sdr/CALA0100886.md): Door Frame · corroded · Sep 19, 2001 · N35836 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED BETWEEN STA 1155-1211. A Z-ANGLE BEAM REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA0000502](https://openairdocs.org/sdr/CALA0000502.md): Acm · leaking · Apr 18, 2000 · N35836 · Doug DC982 · Cabin Cooling System
  > WHEN THROTTLES WERE BROUGHT UP FOR TAKEOFF (DURING TAKEOFF ROLL) A NOXIOUS FOUL ODOR ENTERED THE AIRCRAFT THROUGH THE AIR CONDITIONING PACKS. THE CREW AND PASSENGERS BECAME NAUSEOUS. THE FLIGHT CREW DONNED THEIR O2 MASKS AND THE AIRCRAFT WAS RETURNED TO IAH.
- [SDR CALA0000141](https://openairdocs.org/sdr/CALA0000141.md): Power Supply · inoperative · Feb 8, 2000 · N35836 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. A NEW POWER SUPPLY AND BATTERY PACK WERE INSTALLED IAW MM 33-53-00, PAGE 407.
- [SDR CALA9900538](https://openairdocs.org/sdr/CALA9900538.md): Fairing · gouged · May 13, 1999 · N35836 · Doug DC982 · Leading Edge Devices
  > LEFT WING NR 4 SLAT TRACK CAN GOUGED. WELDED CAN PER DRWG 5935801 AND INSTALLED PER MM 27-80-01.
- [SDR CALA9900527](https://openairdocs.org/sdr/CALA9900527.md): Tail Cone · out of adjust · May 11, 1999 · N35836 · Doug DC982 · Aerodynamic Fairings
  > TAIL COMPARTMENT INTERIOR TAIL CONE RELEASE HANDLE PULL TOO HIGH (45 LBS). RIGGED TAIL CONE RELEASE MECHANISM PER MM 53-53-00.
- [SDR CALA9900525](https://openairdocs.org/sdr/CALA9900525.md): Bracket · cracked · May 11, 1999 · N35836 · Doug DC982 · Emergency Exits
  > LEFT FORWARD EMERGENCY EXIT DOOR SEAL RETAINER SUPPORT BRACKET CRACKED AT RIVET (.5). REPLACED FORWARD LOWER RETAINER BRACKET PER SRM 51-30-2.
- [SDR CALA9900523](https://openairdocs.org/sdr/CALA9900523.md): Skin · gouged · May 11, 1999 · N35836 · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS GOUGED UNDER AFT END OF ADF ANTENNA. BLENDED GOUGE AND INSTALLED REPAIR PER SRM 53-04 FIG 38 VIEW G.
- [SDR CALA9900492](https://openairdocs.org/sdr/CALA9900492.md): Retainer · corroded · May 8, 1999 · N35836 · Doug DC982 · Emergency Exits
  > LEFT FORWARD EMERGENCY EXIT DOOR CORROSION FOUND AT LOWER AFT CORNER SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-30-2.
- [SDR CALA990497](https://openairdocs.org/sdr/CALA990497.md): Jamb · corroded · May 7, 1999 · N35836 · Doug DC982 · Fuselage Miscellaneous Structure
  > FORWARD CORGO DOOR JAMB PAN LOWER SECTION IS CORRODED. INSTALLED SPLICE REPAIR ON DOOR JAMB PER SRM 53-05 FIG 44.
- [SDR CALA9900500](https://openairdocs.org/sdr/CALA9900500.md): Doubler · cracked · May 7, 1999 · N35836 · Doug DC982 · Service Doors
  > AFT SERVICE DOOR DOUBLER AROUND HOLD OPEN HOOK CRACKED (1) OUTER SKIN. INSTALLED DOUBLER REPAIR PER EC/RA 5205-01008.
- [SDR CALA9900496](https://openairdocs.org/sdr/CALA9900496.md): Seat Track · corroded · May 7, 1999 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 2 CORROSION AT NUT PLATE HOLES FROM STA 1136 - 1174. REPLACED SEAT TRACK LEFT CENTER STA 1079 - 1305 PER SRM 51-30-01.
- [SDR CALA9900487](https://openairdocs.org/sdr/CALA9900487.md): Seat Track · corroded · May 5, 1999 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT MOST INBOARD SET TRACK HAS CORROSION AT CENTER CHANNEL STA 1105. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FROM STA 1041 - 1309.
- [SDR CALA9900484](https://openairdocs.org/sdr/CALA9900484.md): Seat Track · corroded · May 4, 1999 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT CENTER SEAT TRACK CORRODED STA 200 AND 237. REMOVED AND REPLACED SEAT TRACK STA 200 - 247 PER SRM 51-30-1.
- [SDR CALA9900470](https://openairdocs.org/sdr/CALA9900470.md): Bulkhead Doubler · corroded · May 3, 1999 · N35836 · Doug DC982 · Fuselage Main, Bulkhead
  > CORROSION AT AFT PRESSURE BULKHEAD AND VERTICAL BULKHEAD INTERSECTION AT STA 1338 FROM L-29LT TO L-29RT. REMOVED CORROSION AND INSTALLED SERVICEABLE JACK PAD DOUBLER PER SRM 51-10-3 AND DRAWING NR PL J936439 AND J936667.
- [SDR CALA9900469](https://openairdocs.org/sdr/CALA9900469.md): Skin · hole · May 3, 1999 · N35836 · Doug DC982 · Fuselage Main, Plate/Skin
  > TEMPORARY REPAIR APPROXIMATELY STA 383 L-29LT WHERE PREVIOUS PHONE ANTENNA INSTALLED. INSTALLED DOUBLERS PER SRM 53-04 FIG 38.
- [SDR CALA9900467](https://openairdocs.org/sdr/CALA9900467.md): Beam · cracked · Apr 30, 1999 · N35836 · Doug DC982 · Service Doors
  > HOU - FORWARD SERVICE DOOR NR 4 BEAM IS CRACKED AT FORWARD END 1.5 INCH. INSTALLED NEW BEAM PER SRM 51-30-2 AND 51-30-1. (M)
- [SDR CALA9900466](https://openairdocs.org/sdr/CALA9900466.md): Beam · cracked · Apr 30, 1999 · N35836 · Doug DC982 · Passenger/Crew Doors
  > HOU - MAIN CABIN DOOR NR 1 BEAM IS CRACKED AT BOTH ENDS.625 INCH FORWARD AND 1 INCH AFT. REMOVED AND REPLACED BEAM PER SRM 51-30-0. (M)
- [SDR CALA9900465](https://openairdocs.org/sdr/CALA9900465.md): Angle · cracked · Apr 30, 1999 · N35836 · Doug DC982 · Vertical Stabilizer
  > HOU - RIGHT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. (M)
- [SDR CALA9900464](https://openairdocs.org/sdr/CALA9900464.md): Angle · cracked · Apr 30, 1999 · N35836 · Doug DC982 · Vertical Stabilizer
  > HOU - LEFT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. (M)
- [SDR CALA9900453](https://openairdocs.org/sdr/CALA9900453.md): Escape Line · frayed · Apr 29, 1999 · N35836 · Doug DC982 · Emergency Equipment
  > RIGHT OVERWING EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00.
- [SDR CALA9900452](https://openairdocs.org/sdr/CALA9900452.md): Escape Line · frayed · Apr 29, 1999 · N35836 · Doug DC982 · Emergency Equipment
  > LEFT OVERWING EMERGENCY EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00.
- [SDR CALA9900223](https://openairdocs.org/sdr/CALA9900223.md): Fuse · blown · Mar 4, 1999 · N35836 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND MIDDLE SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND MOST OUTBOARD FUSE OF MIDDLE POWER SUPPLY PACK BLOWN. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTING WAS RESTORED.
- [SDR CALA9601479](https://openairdocs.org/sdr/CALA9601479.md): Slide · fell off · Oct 17, 1996 · N35836 · Doug DC982 · Emergency Equipment
  > FORWARD ENTRY DOOR SLIDE FELL OFF DOOR. REINSTALLED SLIDE PACK PER MAINTENANCE MANUAL.
- [SDR CAL950187](https://openairdocs.org/sdr/CAL950187.md): T/R Cntl Valve · ruptured · Mar 9, 1995 · N35836 · Doug DC982 · Engine Thrust Reverser
  > SFO - FLT 0165 - THE MAIN CABIN BEGAN TO FILL WITH SMOKE DURING TAXI TO TERMINAL AFTER LANDING AT SFO. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY, THE L-1 DOOR AND TAIL CONE EMERGENCY SLIDES WERE DEPLOYED, AND THE PASSENGERS EVACUATED AS A PRECAUTIONARY MEASURE.

## 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 = 'N35836' AND deregistration_id = 'N35836-2005-06-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N35836-2005-06-29/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.