# Service difficulty reports: N69311, cancelled May 18, 2010

A list on [N69311, cancelled May 18, 2010](https://openairdocs.org/deregistered/N69311-2010-05-18.md).

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

Page 1 of 2 · 92 reports

- [SDR CALA2009101900634](https://openairdocs.org/sdr/CALA2009101900634.md): Battery · discharged · Oct 19, 2009 · N69311 · Boeing 7373T0 · Emergency Lighting
  > R-1 DOOR OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED BATTERY FOR R-1 DOOR EMERGENCY LIGHTS, OPS GOOD.
- [SDR CALA2009012300054](https://openairdocs.org/sdr/CALA2009012300054.md): Skin · cracked · Jan 22, 2009 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FOUND 1.5 INCH LONG SKIN CRACK AT FUSELAGE OUTER SKIN AT 3 INCHES AFT OF STATION 727E AND S-24R. INSTALLED DOUBLER REPAIR, ALL HOLES WERE ZERO TIMED PER SRM 53-00-01, REPAIR 31, PROCEDURE 5. PLACED ON DIP TO INSPECT REPAIR AT 60,000 FLT CYCLES, AFTER REPAIR
- [SDR CALA2009012200052](https://openairdocs.org/sdr/CALA2009012200052.md): Skin · cracked · Jan 21, 2009 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > AFT LEFT FUSELAGE SKIN CRACKED AT APPROX STATION 747 FOUR STRINGERS BELOW LOWER LAP JOINT, CRACK 1.5 INCH LONG. PERFORMED HF EDDY CURRENT IAW NAT 51-00-00 PART 6. REPAIRED PER SRM 53-00-01, REPAIR 31, PROCEDURE V.
- [SDR CALA0700364](https://openairdocs.org/sdr/CALA0700364.md): Attach Fitting · cracked · Jul 17, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN H-STRAP ON FUSELAGE STRUCTURE STA 312 L-1 DOOR LOWER HINGE ATTACH FITTING. A REPAIR WAS INSTALLED IAW ECRA 5311-01342.
- [SDR CALA0700361](https://openairdocs.org/sdr/CALA0700361.md): Skin · corroded · Jul 16, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SKIN STRAP CORRODED AT STA 1006, S27R, BL 0 TO RBL 8. THE CORRODED SECTION OF SKIN STRAP WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01327.
- [SDR CALA0700359](https://openairdocs.org/sdr/CALA0700359.md): Fitting · cracked · Jul 15, 2007 · N69311 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT HORSE COLLAR (FITTING). THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0700358](https://openairdocs.org/sdr/CALA0700358.md): Structure · corroded · Jul 15, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CHORD CORRODED AT STA 227.8, RBL 9 TO LBL 9. A LOWER O/B CHORD REPAIR WAS INSTALLED IAW ECRA 5311-01340.
- [SDR CALA0700354](https://openairdocs.org/sdr/CALA0700354.md): Attach Fitting · cracked · Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK AT AFT END OF ATTACHMENT CLIP, STA 294-309, S10L. THE CLIP WAS REPLACED IAW ECRA 5311-01337.
- [SDR CALA0700353](https://openairdocs.org/sdr/CALA0700353.md): Strap · cracked · Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN H-STRAP AT THE UPPER L-1 DOOR HINGE ATTACH FITTING, STA 312. THE H-STRAP WAS REPLACED IAW ECRA 5311-01337.
- [SDR CALA0700352](https://openairdocs.org/sdr/CALA0700352.md): Frame · cracked · Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.75 INCH CRACK IN STUB FRAME FOR L-2 DOOR UPPER HINGE AREA, STA 947.5, S11L. THE FRAME WAS REPAIRED IAW ECRA 5311-01335.
- [SDR CALA0700351](https://openairdocs.org/sdr/CALA0700351.md): Web · cracked · Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN WEB JUST FORWARD OF L-2 DOOR AT STA 942, S11L. THE CLOSE OUT WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01335.
- [SDR CALA0700350](https://openairdocs.org/sdr/CALA0700350.md): Attach Fitting · cracked · Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK AT I/B CORNER OF ATTACHMENT CLIP, STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01339.
- [SDR CALA0700349](https://openairdocs.org/sdr/CALA0700349.md): Intercostal · cracked · Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL WEB AT RIVET LOCATED AT STA 294.5, S12L. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01339.
- [SDR CALA0700347](https://openairdocs.org/sdr/CALA0700347.md): Stringer · corroded · Jul 11, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED ON FORWARD END BETWEEN STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700343](https://openairdocs.org/sdr/CALA0700343.md): Shear Tie · corroded · Jul 10, 2007 · N69311 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S27R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW MM 51-40-02.
- [SDR CALA0700348](https://openairdocs.org/sdr/CALA0700348.md): Flap Track · corroded · Jul 7, 2007 · N69311 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND CORROSION INSIDE THE AFT TRANSMISSION MOUNT HOLE OF THE NR 8 FLAP TRACK, RT WING, WS 289-511. THE CORROSION IN THE BORE WAS REAMED, SHOT PEENED, PLATED AND A SLEEVE BUSHING WAS INSTALLED IAW CMM 57-53-15, PAGE 16, FIGURE 6 AND SOPM 20-42-10 A
- [SDR CALA0700341](https://openairdocs.org/sdr/CALA0700341.md): Gusset · cracked · Jul 7, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN NOSE WHEEL WELL GUSSET AT END OF NLG DRAG BRACE. THE GUSSET WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700339](https://openairdocs.org/sdr/CALA0700339.md): Door Frame · cracked · Jul 6, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 440, S17R TO 24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700338](https://openairdocs.org/sdr/CALA0700338.md): Pan · cracked · Jul 6, 2007 · N69311 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A.5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED AT EACH CRACK LOCATION IAW ECRA 5210-01941.
- [SDR CALA0700344](https://openairdocs.org/sdr/CALA0700344.md): Fitting · corroded · Jul 3, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 17R END FITTING CORRODED JUST BELOW FLOOR LINE AT STA 1016. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700335](https://openairdocs.org/sdr/CALA0700335.md): Fitting · corroded · Jul 1, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27R END FITTING CORRODED IN BOLT HOLES AT STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700334](https://openairdocs.org/sdr/CALA0700334.md): Fitting · corroded · Jul 1, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L END FITTING CORRODED IN BOLT HOLES, STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-12.
- [SDR CALA0700333](https://openairdocs.org/sdr/CALA0700333.md): Angle · corroded · Jul 1, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD FACE LOWER CHORD ANGLE CORRODED AT STA 1016 FROM S27L T0 S27R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700331](https://openairdocs.org/sdr/CALA0700331.md): Door Frame · cracked · Jun 30, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 440. THE FORWARD FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700330](https://openairdocs.org/sdr/CALA0700330.md): Pressure Panel · cracked · Jun 29, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51 AND 51-40-02.
- [SDR CALA0700329](https://openairdocs.org/sdr/CALA0700329.md): Web · corroded · Jun 28, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED FROM STA 986.5 TO 1006, S21R. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40-02.
- [SDR CALA0700327](https://openairdocs.org/sdr/CALA0700327.md): Floorbeam · corroded · Jun 27, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 986.5, LBL 43. THE CORRODED T-CHORD SECTION OF BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700326](https://openairdocs.org/sdr/CALA0700326.md): Floorbeam · corroded · Jun 27, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND SURFACE CORROSION AROUND SCREW HOLES ON FLOORBEAM AT STA 1016 FROM LBL 30 TO LBL 34, S19L-S21L. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51.
- [SDR CALA0700324](https://openairdocs.org/sdr/CALA0700324.md): Fitting · cracked · Jun 26, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 0.65 INCH CRACK IN CLIP AT STA 616, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700323](https://openairdocs.org/sdr/CALA0700323.md): Fitting · cracked · Jun 26, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN CLIP AT STA 597, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600005](https://openairdocs.org/sdr/CALA0600005.md): Spar · corroded · Jan 10, 2006 · N69311 · Boeing 7373T0 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND THE LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP CORRODED FROM STAB STA 196.2 TO 200.3. THE LT HORIZONTAL STABILIZER ASSEMBLY WAS REMOVED AND REPLACED MM 27-41-11, PAGE 401, FIGURE 401.
- [SDR CALA0600002](https://openairdocs.org/sdr/CALA0600002.md): Skin · cracked · Jan 8, 2006 · N69311 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.
- [SDR CALA0400683](https://openairdocs.org/sdr/CALA0400683.md): Skin · cracked · Oct 22, 2004 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.8 INCH CRACK IN FUSELAGE SKIN 3 INCHES AFT OF STA 727D AND BELOW S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090.
- [SDR CALA0300525](https://openairdocs.org/sdr/CALA0300525.md): Keelbeam · corroded · Sep 11, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LIGHT CORROSION ON O/B FLANGE OF LEFT KEELBEAM FROM BS 663-727. INSTALLED REPAIR IAW ECRA 5311-01167.
- [SDR CALA0300529](https://openairdocs.org/sdr/CALA0300529.md): Floorbeam · corroded · Sep 5, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION ALONG THE ENTIRE UPPER SECTION OF FLOORBEAM AT STA 967. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142.
- [SDR CALA0300514](https://openairdocs.org/sdr/CALA0300514.md): Fitting · cracked · Sep 5, 2003 · N69311 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN LT WING UPPER AFT INBOARD T/E PANEL OUTBOARD SUPPORT FITTING. A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300513](https://openairdocs.org/sdr/CALA0300513.md): Cargo Track · corroded · Sep 4, 2003 · N69311 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN RAIL CORRODED AT FASTENERS ON LOWER SURFACE AT STA 947 IN THE AFT CARGO COMPARTMENT. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53.
- [SDR CALA0300510](https://openairdocs.org/sdr/CALA0300510.md): Frame · corroded · Sep 3, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND CORROSION ON FRAME AT STA 793 BETWEEN S26R AND S25R IN AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA0300509](https://openairdocs.org/sdr/CALA0300509.md): Angle · cracked · Sep 3, 2003 · N69311 · Boeing 7373T0 · Nacelle/Pylon, Main Frame
  > INSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300507](https://openairdocs.org/sdr/CALA0300507.md): Bracket · cracked · Aug 30, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.2500 INCH CRACK IN VHF RIGHT FORWARD SUPPORT AFT CARGO COMPARTMENT BRACKET AT STA 727D. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300506](https://openairdocs.org/sdr/CALA0300506.md): Shear Tie · corroded · Aug 30, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD BAGGAGE BIN SKIN SHEAR TIE CORRODED AT STA 460, S28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR DOUBLER AND SHEAR TIE WERE INSTALLED IAW SRM 53-00-07.
- [SDR CALA0300505](https://openairdocs.org/sdr/CALA0300505.md): Floor Panel · cracked · Aug 29, 2003 · N69311 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND A 1 INCH AND.5000 INCH CRACK IN AFT BAGGAGE BIN FLOOR PANEL 1536X AT STA 794.5-807. A DOUBLER WAS INSTALLED AT EACH CRACK LOCATION IAW SRM 53-30-53.
- [SDR CALA0300504](https://openairdocs.org/sdr/CALA0300504.md): Door Frame · cracked · Aug 29, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A 7.5 INCH CRACK IN FORWARD BAGGAGE BIN WEB AT FORWARD LOWER DOOR JAMB, STA 440. A NEW SECTION OF WEB WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0300503](https://openairdocs.org/sdr/CALA0300503.md): Support · cracked · Aug 29, 2003 · N69311 · Boeing 7373T0 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5000 INCH CRACK IN RT WING UPPER MOST I/B T/E PANEL SUPPORT. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300502](https://openairdocs.org/sdr/CALA0300502.md): Galley Track · corroded · Aug 28, 2003 · N69311 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND NR 3 GALLEY I/B AFT MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300501](https://openairdocs.org/sdr/CALA0300501.md): Frame · cracked · Aug 27, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616. A DOUBLER ANGLE WAS INSTALLED IAW ECRA 5311-01158.
- [SDR CALA0300500](https://openairdocs.org/sdr/CALA0300500.md): Stiffener · gouged · Aug 27, 2003 · N69311 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 6 FLAP TRACK FAIRING I/B STIFFENER GOUGED. THE STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300498](https://openairdocs.org/sdr/CALA0300498.md): Bracket · corroded · Aug 26, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON CORNER BRACKET O/B OF DOOR CUTOUT RT AFT CORNER FWD ACC COMPT, STA 219. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300497](https://openairdocs.org/sdr/CALA0300497.md): Floor Support · corroded · Aug 26, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER AND LOWER SURFACE OF FLOOR SUPPORT CORRODED BETWEEN STA 967 AND 986.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0300494](https://openairdocs.org/sdr/CALA0300494.md): Angle · corroded · Aug 25, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT BS 947-986, LBL 48. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Next page: https://openairdocs.org/deregistered/N69311-2010-05-18/reports.md?page=2

## 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 = 'N69311' AND deregistration_id = 'N69311-2010-05-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N69311-2010-05-18/reports

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