# Service difficulty reports: N10323, cancelled Apr 28, 2011

A list on [N10323, cancelled Apr 28, 2011](https://openairdocs.org/deregistered/N10323-2011-04-28.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 · 59 reports

- [SDR CALA2009050700246](https://openairdocs.org/sdr/CALA2009050700246.md): Downlock Sensor · failed · May 7, 2009 · N10323 · Boeing 7373T0 · Landing Gear Position and Warning
  > IN FLIGHT WITH THE LANDING GEAR UP, THE GREEN NOSE GEAR LIGHT WOULD FLASH INTERMITTENTLY. TROUBLESHOT PER M/M 32-61-00, FOUND NLG DOWN LOCK SENSOR RED TO YELLOW OPEN, REF WDM 32-64-01 PG 1 OF 2. REMOVED AND REPLACED S-845 PER M/M 32-61-51, PG 401-407. FUNCT
- [SDR CALA2009021000091](https://openairdocs.org/sdr/CALA2009021000091.md): Charger · inoperative · Feb 10, 2009 · N10323 · Boeing 7373T0 · Emergency Lighting
  > DURING CHECK OF EMERGENCY LIGHTING, R1 DOOR EMERGENCY EXIT SIGN DID NOT ILLUMINATE. T/S PER WDM 33-51-31 PG 1. FOUND BATTERY CHARGER INOPERATIVE AT STATION 338R. REMOVED AND REPLACED BATTERY AND CHARGER PER MM 33-51-51. EMERGENCY LIGHTING SYSTEM OPS CHECKS
- [SDR CALA0700294](https://openairdocs.org/sdr/CALA0700294.md): Skin · corroded · Jun 6, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SKIN AT TOP ATC ANTENNA MOUNTING SURFACE CORRODED, STA 420-440, S1L TO 2L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. A DIP WAS INITIATED TO COMPLY WITH ECRA 5330-03685 STEP 6 ON OR BEFORE JUNE 4, 2008 AND TO PERFORM A PERMANENT RE
- [SDR CALA0700288](https://openairdocs.org/sdr/CALA0700288.md): Keelbeam · corroded · Jun 3, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND RIGHT KEELBEAM CORRODED JUST INSIDE A/C BAY AT STA 537. THE KEELBEAM WAS REPAIRED IAW SRM 53-60-12.
- [SDR CALA0700278](https://openairdocs.org/sdr/CALA0700278.md): Frame · cracked · Jun 2, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700287](https://openairdocs.org/sdr/CALA0700287.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 5 INCH CRACK IN AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER DOOR STOP AREA, STA 947.5, S16R-26R. THE FRAME WAS REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-20723, AND ECRA 5311-01323.
- [SDR CALA0700286](https://openairdocs.org/sdr/CALA0700286.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700285](https://openairdocs.org/sdr/CALA0700285.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 847 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700284](https://openairdocs.org/sdr/CALA0700284.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 867 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700283](https://openairdocs.org/sdr/CALA0700283.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 827 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700282](https://openairdocs.org/sdr/CALA0700282.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700281](https://openairdocs.org/sdr/CALA0700281.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 807 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700280](https://openairdocs.org/sdr/CALA0700280.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 747 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700279](https://openairdocs.org/sdr/CALA0700279.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 827 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700277](https://openairdocs.org/sdr/CALA0700277.md): Frame · cracked · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE FRAME AT STA 867, S8L-9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636.
- [SDR CALA0700276](https://openairdocs.org/sdr/CALA0700276.md): Skin · corroded · Jun 1, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND MOUNTING SKIN SURFACE FOR NR 2 COMM ANTENNA CORRODED AT STA 480-500B, S28L TO S28R. THE SKIN WAS REPAIRED IAW ECRA 5331-01316.
- [SDR CALA0700269](https://openairdocs.org/sdr/CALA0700269.md): Frame · corroded · May 27, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND LOWER O/B CHORD CORRODED AT STA 227, RBL 0 TO LBL 3. REPAIRED IAW ECRA 5311-01324 ITEM 1-16, PAGE 1-3.
- [SDR CALA0700267](https://openairdocs.org/sdr/CALA0700267.md): Door Frame · cracked · May 26, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A.75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 480-500, S16R TO S28R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02, PARAGRAPHS 4 AND 7.
- [SDR CALA0700265](https://openairdocs.org/sdr/CALA0700265.md): Shear Tie · corroded · May 25, 2007 · N10323 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND RIGHT NLG WW SHEAR TIE CORRODED AT STA 285. A REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700262](https://openairdocs.org/sdr/CALA0700262.md): Shear Tie · corroded · May 24, 2007 · N10323 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND RIGHT NLG WW CHORD SHEAR TIE CORRODED AT STA 275, S25R-S26R. A SHEAR TIE FILLER REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700257](https://openairdocs.org/sdr/CALA0700257.md): Frame · corroded · May 22, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 312, RBL 2, S27R-28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 1.
- [SDR CALA0700255](https://openairdocs.org/sdr/CALA0700255.md): Frame · corroded · May 22, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 312, S28L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-02 AND 53-00-07.
- [SDR CALA0700254](https://openairdocs.org/sdr/CALA0700254.md): Stringer · corroded · May 21, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R CORRODED AT STA 325. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-20-01 AND 51-70-13.
- [SDR CALA0700253](https://openairdocs.org/sdr/CALA0700253.md): Frame · cracked · May 18, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT MAIN FRAME AT STA 616, S17L, BELOW MAIN DECK FLOOR. THE FRAME WAS REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0700248](https://openairdocs.org/sdr/CALA0700248.md): Angle · corroded · May 15, 2007 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE AT R-2 DOOR ENTRYWAY, STA 947.5-1000, S17R, CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700246](https://openairdocs.org/sdr/CALA0700246.md): Angle · corroded · May 15, 2007 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE AT L-2 DOOR, STA 907-1006, LBL 50 CORRODED. THE Z-ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700242](https://openairdocs.org/sdr/CALA0700242.md): Floorbeam · corroded · May 13, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT FLOORBOARD MOUNT HOLES, STA 967, S17L TO S17R. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIGURE 201, PAGE 201.
- [SDR CALA0700241](https://openairdocs.org/sdr/CALA0700241.md): Floorbeam · corroded · May 13, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 43-54. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700238](https://openairdocs.org/sdr/CALA0700238.md): Floorbeam · corroded · May 9, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 32-34. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.
- [SDR CALA0700258](https://openairdocs.org/sdr/CALA0700258.md): Skin · cracked · May 8, 2007 · N10323 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AROUND L-2 DOOR LOWER HINGE CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-60-01.
- [SDR CALA0400436](https://openairdocs.org/sdr/CALA0400436.md): Wire · shorted · Apr 28, 2004 · N10323 · Boeing 7373T0 · Light System Wiring
  > EMERGENCY LIGHTS INOP AT SEAT ROWS 5-12. REPAIRED SHORTED WIRE UNDER SEAT ROW 5 PER STANDARD PRACTICES MANUAL.
- [SDR CALA0300283](https://openairdocs.org/sdr/CALA0300283.md): Skin · cracked · May 21, 2003 · N10323 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND THE AFT CARGO DOOR INNER SKIN CRACKED AT THE EDGE OF A LIGHTENING HOLE. THE DOOR SKIN WAS REPAIRED IAW ECRA 5232-01029.
- [SDR CALA0300263](https://openairdocs.org/sdr/CALA0300263.md): Skin · cracked · May 21, 2003 · N10323 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1/2 INCH CRACK IN C-2 DOOR INNER SKIN AT ACCESS PANEL CUTOUT BELOW HANDLE. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01029.
- [SDR CALA0300256](https://openairdocs.org/sdr/CALA0300256.md): Skin · cracked · May 19, 2003 · N10323 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN C-2 DOOR INNER SKIN ABOVE HANDLE ON LIGHTENING HOLE. THE SKIN WAS REPAIRED IAW ECRA 5232-01015.
- [SDR CALA0300251](https://openairdocs.org/sdr/CALA0300251.md): Channel · corroded · May 15, 2003 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND U-CHANNEL FOR DRAIN MAST CORRODED AT STA 986.5 BETWEEN S24L AND S25L. INSTALLED DRAIN MAST IAW MM 30-71-00, PAGE 501-503.
- [SDR CALA0300248](https://openairdocs.org/sdr/CALA0300248.md): Stiffener · corroded · May 14, 2003 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STIFFENER AFT OF STA 1016, BL 0 CORRODED ON BOTH RIGHT AND LEFT SIDES. LEFT AND RIGHT STIFFENERS AND SPLICES WERE INSTALLED IAW EA 5310-04045 AND DRAWING 65C28106.
- [SDR CALA0300247](https://openairdocs.org/sdr/CALA0300247.md): Stringer · corroded · May 14, 2003 · N10323 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-01.
- [SDR CALA0300245](https://openairdocs.org/sdr/CALA0300245.md): Angle · corroded · May 12, 2003 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR ENTRYWAY Z-ANGLE CORRODED AT STA 943-987. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-2.
- [SDR CALA0300241](https://openairdocs.org/sdr/CALA0300241.md): Bulkhead · corroded · May 12, 2003 · N10323 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD CORRODED JUST AFT OF FS 1016 AT LBL 6 TO RBL 6. REPAIRED APB IAW DRAWING 65C28106-1.
- [SDR CALA0300236](https://openairdocs.org/sdr/CALA0300236.md): Floor Support · corroded · May 9, 2003 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 992-1006, RBL 7. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300160](https://openairdocs.org/sdr/CALA0300160.md): Skin · damaged · Mar 28, 2003 · N10323 · Boeing 7373T0 · Horizontal Stabilizer Structure
  > WHILE PERFORMING A PERMANENT REPAIR OF THE LT HORIZONTAL STABILIZER LE SKIN AT LE STA 69.93 IN IAH PER SRM 55-10-01, FIGURE 203, MAINTENANCE NOTED THE REQUIRED FLUSH REPAIR WAS NOT APPLICABLE TO THIS AREA BECAUSE THE DAMAGED AREA WAS CLOSE TO A RIB. THE REPAIR
- [SDR CALA0100934](https://openairdocs.org/sdr/CALA0100934.md): Skin · dented · Oct 5, 2001 · N10323 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND L/H HORIZONTAL STABILIZER L/E SKIN DENTED AT STA 147.90. A REPAIR WAS INSTALLED IAW ECRA 5510-01602.
- [SDR CALA0100931](https://openairdocs.org/sdr/CALA0100931.md): Skin · gouged · Oct 4, 2001 · N10323 · Boeing 7373T0 · Rudder, Plate/Skin
  > INSPECTION FOUND R/H RUDDER L/E SKIN GOUGED BELOW ACCESS PANEL 9559. REPAIRED IAW SRM 51-70-17 AND ECRA 5543-01017.
- [SDR CALA0100927](https://openairdocs.org/sdr/CALA0100927.md): Skin · dented · Oct 3, 2001 · N10323 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND THE L/H HORIZONTAL STABILIZER FIXED L/E SKIN DENTED AT SECOND RIB FROM I/B. A REPAIR WAS INSTALLED IAW SRM 55-10-01, PAGE 202.
- [SDR CALA0100924](https://openairdocs.org/sdr/CALA0100924.md): Angle · dented · Oct 2, 2001 · N10323 · Boeing 7373T0 · Auxiliary Power Unit (APU) Doors
  > INSPECTION FOUND APU DOOR ANGLE DENTED ON AFT EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0100910](https://openairdocs.org/sdr/CALA0100910.md): Web · corroded · Sep 30, 2001 · N10323 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED AROUND FASTENERS AT LOWER SIDE OF C-2 DOOR UPPER THRESHOLD. A NEW WEB WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0100907](https://openairdocs.org/sdr/CALA0100907.md): Keelbeam · corroded · Sep 29, 2001 · N10323 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM CORRODED ON LOWER SURFACE AT STA 705-727, LT SIDE. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03740.
- [SDR CALA0100546](https://openairdocs.org/sdr/CALA0100546.md): Bolt · cracked · Jun 15, 2001 · N10323 · Boeing 7373T0 · Landing Gear Doors
  > INSPECTION FOUND BOTH RT LANDING GEAR DOOR TO STABILIZER BEAM BOLTS PITTED AND ONE BOLT HAD A.25 INCH CRACK. NEW BOLTS, WASHERS, AND NUTS WERE INSTALLED IAW MM 32-00-00.
- [SDR CALA0100545](https://openairdocs.org/sdr/CALA0100545.md): Bolt · cracked · Jun 15, 2001 · N10323 · Boeing 7373T0 · Landing Gear Doors
  > INSPECTION FOUND BOTH LT LANDING GEAR DOOR TO STABILIZER BEAM BOLTS PITTED AND CRACKED. THE CRACKS WERE.25 INCH LONG. NEW BOLTS, WASHERS, AND NUTS WERE INSTALLED IAW MM 32-00-00.
- [SDR CALA0100397](https://openairdocs.org/sdr/CALA0100397.md): Warn Panel · faulty · Apr 18, 2001 · N10323 · Boeing 7373T0 · Fire Detection
  > THE CARGO FIRE LIGHT ILLUMINATED WHILE EN ROUTE FROM IAH TO YYZ. NO BELL SOUNDED. THE CARGO FIRE SYSTEM TESTED NORMALLY, BUT THE LIGHT REMAINED ON AFTER TEST. RESET ALL CIRCUIT BREAKERS FOR CARGO FIRE SYSTEM, BUT THE FIRE LIGHT WOULD NOT GO OUT. THE AIRCAR

Next page: https://openairdocs.org/deregistered/N10323-2011-04-28/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 = 'N10323' AND deregistration_id = 'N10323-2011-04-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10323-2011-04-28/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.