# Service difficulty reports: N39343, cancelled Aug 21, 2009

A list on [N39343, cancelled Aug 21, 2009](https://openairdocs.org/deregistered/N39343-2009-08-21.md).

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

- [SDR CALA0800478](https://openairdocs.org/sdr/CALA0800478.md): Shear Tie · corroded · May 21, 2008 · N39343 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > STATION 967 BETWEEN S27L AND S27R FRAME CORRODED. REPAIRED SHEAR TIE AT SKIN ATTACHMENTS REF SRM 53-00-07 FIG 201, REPAIR 1.
- [SDR CALA0800482](https://openairdocs.org/sdr/CALA0800482.md): Bulkhead · cracked · May 20, 2008 · N39343 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > LEFT-HAND MLG WHEEL WELL PRESSURE DECK CRACKED AT UPPER FWD SKIN LOCATED APPROXIMATELY LBL 40. REPAIRED IAW SRM 53-60-51 REPAIR 4.
- [SDR CALA0800413](https://openairdocs.org/sdr/CALA0800413.md): Skin · damaged · May 1, 2008 · N39343 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FOUND SKIN DAMAGED 2 FT AFT OF LEFTHAND AFT WING TO BODY FAIRING JUST BELOW SPLICE BELT APP STATION 727. REPAIRED IN REFERENCE SRM 53-00-01 REPAIR 31 AS REQUIRED.
- [SDR CALA0600470](https://openairdocs.org/sdr/CALA0600470.md): Stringer · corroded · Nov 12, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED AT STA 493. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0600468](https://openairdocs.org/sdr/CALA0600468.md): Stringer · corroded · Nov 12, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED AT STA 500-500A. A STRINGER REPAIR WAS INSTALLED SRM 53-00-03.
- [SDR CALA0600458](https://openairdocs.org/sdr/CALA0600458.md): Attach Angle · cracked · Nov 10, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN RT INTERCOSTAL ATTACH ANGLE AT STA 277 BETWEEN S14R AND S13R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0600457](https://openairdocs.org/sdr/CALA0600457.md): Attach Angle · cracked · Nov 10, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN RT INTERCOSTAL ATTACH ANGLE AT STA 294, S11R. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0600455](https://openairdocs.org/sdr/CALA0600455.md): Frame · cracked · Nov 10, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN AFT LOWER FRAME AFT OF UPPER BOLT HOLE FOR LOWER DOOR STOP, STA 500, S21R. A NEW FRAME WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0600453](https://openairdocs.org/sdr/CALA0600453.md): Seat Track · corroded · Nov 10, 2006 · N39343 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 919, RBL 20. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0600451](https://openairdocs.org/sdr/CALA0600451.md): Floorbeam · corroded · Nov 7, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT ENTRY FLOORBEAM FLANGE CORRODED AT STA 947, RBL 22 TO LBL 5. A NEW SECTION OF FLOORBEAM UPPER FLANGE WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.
- [SDR CALA0600485](https://openairdocs.org/sdr/CALA0600485.md): Attach Angle · cracked · Nov 5, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL ATTACH ANGLE AT STA 294, BETWEEN S10R AND S11R. THE ATTACH ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0600459](https://openairdocs.org/sdr/CALA0600459.md): Attach Angle · cracked · Nov 5, 2006 · N39343 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN RT INTERCOSTAL ATTACH ANGLE AT STA 294, S10R. THE ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0600450](https://openairdocs.org/sdr/CALA0600450.md): Intercostal · cracked · Nov 4, 2006 · N39343 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN INTERCOSTAL AT STA 277, S14L. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0700032](https://openairdocs.org/sdr/CALA0700032.md): Cooling Fan · failed · Oct 30, 2006 · N39343 · Boeing 7373T0 · Air Distribution Fan
  > A SMOKY ODOR WAS NOTICED IN THE COCKPIT AND CABIN AND THE EQ COOLING LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO SFO. THE RECIRC FAN SWITCH WAS TURNED OFF AND THE ODOR WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE BLOWER CIR
- [SDR CALA0400032](https://openairdocs.org/sdr/CALA0400032.md): Pressure Panel · damaged · Jan 9, 2004 · N39343 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND DAMAGE TO THE PRESSURE DECK WEB AT STA 665 TO 675, RBL 35 TO 45. THE PRESSURE WEB DECK WAS REPAIRED IAW ECRA 5312-01023.
- [SDR CALA0200549](https://openairdocs.org/sdr/CALA0200549.md): Floorbeam · corroded · Nov 13, 2002 · N39343 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 967, RBL 46. OLD TOP CHORD REPAIR EXISTS FROM LBL 43 TO RBL 43. FLOORBEAM REPAIRED IAW ECRA 5311-01142. TOP CHORD REPLACED FROM LBL 43 TO R/H EXTREMITY AT FRAME.
- [SDR CALA0200531](https://openairdocs.org/sdr/CALA0200531.md): Skin · dented · Nov 6, 2002 · N39343 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR SKIN DENTED AT 35" FROM TOP AND 10" FROM FORWARD EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
- [SDR CALA0200527](https://openairdocs.org/sdr/CALA0200527.md): Skin · Nov 4, 2002 · N39343 · Boeing 7373T0 · Fuselage Structure (General)
  > FUSELAGE SKIN CRACKED AT AFT SCREW HOLE LOWER FUSELAGE CENTER LINE STA 380 AT EXHAUST OUTLET. INSTALLED DOUBLER IAW ECRA 5330-02894
- [SDR CALA0200517](https://openairdocs.org/sdr/CALA0200517.md): Frame · cracked · Oct 31, 2002 · N39343 · Boeing 7373T0 · Fuselage Main, Frame
  > BS FRAME 616 CRACKED LBL 65 WL 200 I/B CHORD BELOW CABIN FLOOR LINE. INSTALLED REPAIR FILLER AND ANGLE PER ECRA 5311-01141.
- [SDR CALA0200516](https://openairdocs.org/sdr/CALA0200516.md): Floor Support · Oct 30, 2002 · N39343 · Boeing 7373T0 · Fuselage Structure (General)
  > CABIN FLOOR R/H DIAGONAL SUPPORT HAS CORROSION ON TOP SHIM AT STA 987-1006. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.
- [SDR CALA0200515](https://openairdocs.org/sdr/CALA0200515.md): Angle · cracked · Oct 29, 2002 · N39343 · Boeing 7373T0 · Wing Miscellaneous Structure
  > SUPPORT ANGLE CRACKED TWO PLACES FORWARD OF NR 3 FLAP TRACK FAIRING. REPLACED SUPPORT COLLAR ANGLE PER SRM 51-40-02.
- [SDR CALA0200514](https://openairdocs.org/sdr/CALA0200514.md): Stiffener · worn · Oct 29, 2002 · N39343 · Boeing 7373T0 · Wing Miscellaneous Structure
  > HOCKEY STICK WORN IB EDGE OF NR 3 FLAP TRACK FAIRING. REPLACED HOCKEY STICK IB EDGE OF NR 3 FLAP TRACK FAIRING PER SRM 51-40-02.
- [SDR CALA0200513](https://openairdocs.org/sdr/CALA0200513.md): Web · Oct 29, 2002 · N39343 · Boeing 7373T0 · Lavatories
  > VERTICAL WEB CRACKED AT STA 1016 LBL 4. INSTALLED WEB AT STA 1016, LBL4 PER SRM 51-40-02.
- [SDR CALA0200512](https://openairdocs.org/sdr/CALA0200512.md): Channel · Oct 29, 2002 · N39343 · Boeing 7373T0 · Fuselage Main, Structure
  > CORROSION ON ANTENNA DOUBLER BETWEEN STA 500-500A, BL0. REMOVED AND REPLACED DOUBLER PER SRM 51-10-02.
- [SDR CALA0200509](https://openairdocs.org/sdr/CALA0200509.md): Stringer · Oct 27, 2002 · N39343 · Boeing 7373T0 · Fuselage Main, Structure
  > CRACK IN STRINGER 16R FORWARD OF LIGHT AT APPROXIMATELY 500B. INSTALLED NEW STRINGER AND DOUBLER PER SRM 53-00-03.
- [SDR CALA0200508](https://openairdocs.org/sdr/CALA0200508.md): Bulkhead · corroded · Oct 26, 2002 · N39343 · Boeing 7373T0 · Fuselage Main, Structure
  > AFT PRESSURE BULKHEAD SKIN AT STA. 1016 UNDER RT STIFFENER CORRODED AT BL0. INSTALLED DOUBLER PER EA 5310-04045.
- [SDR CALA0200505](https://openairdocs.org/sdr/CALA0200505.md): Floor Support · corroded · Oct 24, 2002 · N39343 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200504](https://openairdocs.org/sdr/CALA0200504.md): Floorbeam · corroded · Oct 23, 2002 · N39343 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 967, LBL 6 TO RBL 6. A STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51.
- [SDR CALA0200503](https://openairdocs.org/sdr/CALA0200503.md): Floor Support · corroded · Oct 23, 2002 · N39343 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328-344, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0101024](https://openairdocs.org/sdr/CALA0101024.md): Control Panel · faulty · Dec 8, 2001 · N39343 · Boeing 7373T0 · Fire Detection
  > A CARGO FIRE WARNING LIGHT ILLUMINATED AT FL 330 WHILE EN ROUTE FROM PHX TO IAH. BOTH FIRE BOTTLES WERE DISCHARGED IAW QRH PROCEDURES AND THE FLIGHT WAS DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. TROUBLESHOOTING
- [SDR CALA9802080](https://openairdocs.org/sdr/CALA9802080.md): Seat Track · corroded · Nov 18, 1998 · N39343 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT STA 927, LBL 25. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-00-52.
- [SDR CALA9802067](https://openairdocs.org/sdr/CALA9802067.md): Floorbeam · corroded · Nov 16, 1998 · N39343 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT BS 328, LBL 50 TO RBL 50. THE CORRODED AREA WAS REMOVED AND AN UPPER CHORD REPAIR SPLICE WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA9802057](https://openairdocs.org/sdr/CALA9802057.md): Floorbeam · corroded · Nov 11, 1998 · N39343 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. REPAIRED IAW ECRA 5310-03450.
- [SDR CALA9800949](https://openairdocs.org/sdr/CALA9800949.md): Seat Track · corroded · Jun 2, 1998 · N39343 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CORROSION ON RT INBOARD SEAT TRACK BETWEEN STA 915 AND 937. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52.
- [SDR CALA9600924](https://openairdocs.org/sdr/CALA9600924.md): Flt Contl Comp · inoperative · Jun 28, 1996 · N39343 · Boeing 7373T0 · Flight Management Computing Hardware System
  > THE AUTOPILOT DISENGAGED FOLLOWED BY ILLUMINATION OF STAB OUT OF TRIM LIGHT, SPEED TRIM FAIL LIGHT, MACH TRIM FAIL LIGHT, OFF FLAGS IN CAPTAIN'S AIRSPEED, ALTITUDE AND VVI INDICATORS AND CAPTAIN'S FLIGHT DIRECTOR V-BARS VIBRATING DURING CRUISE FLIGHT. TROUBLE
- [SDR CAL950877](https://openairdocs.org/sdr/CAL950877.md): Coupler · failed · Oct 2, 1995 · N39343 · Boeing 7373T0 · Autopilot System
  > CLE - FLT 0288 - THE YAW DAMPER STARTED KICKING RUDDER BACK AND FORTH AT FL330. THE KICKING STOPPED WHEN YAW DAMPER WAS TURNED OFF. SHORTLY AFTER TURNING OFF YAW DAMPER, ACFT MADE 2 UNCOMMANDED ROLLS TO THE RIGHT WITH 'B' AUTOPILOT ENGAGED IN 'L-NAV, V-NAV'

## 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 = 'N39343' AND deregistration_id = 'N39343-2009-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N39343-2009-08-21/reports

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