# Service difficulty reports: N59338, cancelled Mar 21, 2013

A list on [N59338, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N59338-2013-03-21.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 · 70 reports

- [SDR CALA2009072200387](https://openairdocs.org/sdr/CALA2009072200387.md): Windshield · cracked · Jul 22, 2009 · N59338 · Boeing 7373T0 · Flight Compartment Windows
  > WHILE AT CRUISE SAW WINDOW R-1 HAVE AN ELECTRICAL ARC OFF WINDOW HEAT CIRCUITRY AND OUTER PANE CRACKED SEVERAL PLACES. PERFORMED QRH PROCEDURE, TURNED OFF RT WINDOW HEAT AND PROCEEDED TO IAH. REMOVED AND REPLACE DR-1 WINDSHIELD PER AMM 56-11-11-004-001 AND 5
- [SDR CALA2009060100283](https://openairdocs.org/sdr/CALA2009060100283.md): Stringer · corroded · May 27, 2009 · N59338 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS HEAVY CORROSION DIRECTLY BELOW LAV TANK AT STATION 967 AT BL 0. INSTALLED REPAIR REF SRM 53-00-03, REPAIR 1.
- [SDR CALA2009051400255](https://openairdocs.org/sdr/CALA2009051400255.md): Cable · frayed · May 10, 2009 · N59338 · Boeing 7373T0 · Escape Slide
  > L-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED L-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE REF 737 AMM25-61-35.
- [SDR CALA2009012600058](https://openairdocs.org/sdr/CALA2009012600058.md): Skin · dented · Jan 24, 2009 · N59338 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > DENT ON RIGHT SIDE OF AIRCRAFT AT APPROXIMATELY STATION 931 FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, PG 103V, U / PG 106 DETAIL III. REPAIRED PER ECRA 5331-01399, SRM 53-00-01 REPAIR 31, FIG 201, PROC V. INITIATED DIP TO ACCOMPLISH PERMANENT REPAIR BEFORE
- [SDR CALA0800249](https://openairdocs.org/sdr/CALA0800249.md): Sill · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > SILL ASSEMBLY AT STA 303.9 FORWARD LATERAL FRAME CRACKED. REMOVED AND REPLACED SILL AT STA 303.9 PER SRM 51-40-02.
- [SDR CALA0800248](https://openairdocs.org/sdr/CALA0800248.md): Stringer Splice · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE CHANNEL AT STRINGER 14L BETWEEN STA 350 AND 360 CRACKED. REMOVED AND REPLACED SPLICE CHANNEL PER ECRA 5311-01400.
- [SDR CALA0800247](https://openairdocs.org/sdr/CALA0800247.md): Stringer · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > STRINGER 16L U-CHANNEL CRACKED AT STA 360. REMOVED AND REPLACED U-CHANNEL PER ECRA 5311-01400.
- [SDR CALA0800246](https://openairdocs.org/sdr/CALA0800246.md): Attach Fitting · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > ATTACHING CLIP AT STRINGER 11L BETWEEN BS 350 AND 360 CRACKED. REMOVED AND INSTALLED NEW CLIP PER ECRA 5311-01400.
- [SDR CALA0800245](https://openairdocs.org/sdr/CALA0800245.md): Attach Fitting · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > ATTACHING CLIP AT STRINGER 8L BETWEEN BS 350 AND 360 CRACKED. REMOVED AND INSTALLED NEW CLIP PER ECRA 5311-01400.
- [SDR CALA0800244](https://openairdocs.org/sdr/CALA0800244.md): Intercostal · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > THE 7L INTERCOSTAL FORWARD OF STA 294.5 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER ECRA 5311-01400.
- [SDR CALA0800243](https://openairdocs.org/sdr/CALA0800243.md): Attach Fitting · cracked · Mar 21, 2008 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CLIP ON FORWARD END BOTTOM SIDE OF INTERCOSTAL AT STA 15L THAT ATTACHES INTERCOSTAL TO 348.2 FRAME HAS.875 INCH CRACK IN RADIUS AT I/B END. REMOVED AND REPLACED CLIP PER ECRA 5311-01400.
- [SDR CALA0800237](https://openairdocs.org/sdr/CALA0800237.md): Beltframe · corroded · Mar 18, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT CARGO BILGE AREA - CORROSION AT BELT FRAME, STA 807, APPROX LBL 24. REMOVED CORROSION AND INSTALLED REPAIR AT STA 807 APPROX LBL 24 REF SRM 53-00-07.
- [SDR CALA0800236](https://openairdocs.org/sdr/CALA0800236.md): Frame · corroded · Mar 18, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT CARGO BILGE AREA - CORROSION ON FRAME AT STA 727E APPROX LBL 24. FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED REF SRM 53-00-07 REPAIR 5.
- [SDR CALA0800231](https://openairdocs.org/sdr/CALA0800231.md): Skin · cracked · Mar 17, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > R-1 DOOR CUTOUT LWR AFT CORNER CRACKED APPROX 1.5 INCH LONG. INSTALLED REPAIR REF SRM 53-10-01 REPAIR 2.
- [SDR CALA0800229](https://openairdocs.org/sdr/CALA0800229.md): Stringer Clip · cracked · Mar 17, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > STRINGER CLIP AT STRINGER 4L STA 380 CRACKED. REMOVED AND REPLACED STRINGER CLIP REF SRM 51-40-02.
- [SDR CALA0800228](https://openairdocs.org/sdr/CALA0800228.md): Stringer · damaged · Mar 17, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > STRINGER 4-L DAMAGED AT STA 380. REMOVED DAMAGED SECTION OF STRINGER FROM A/C AND SPLICED IN NEW. REF SRM 53-00-03 REPAIR 3.
- [SDR CALA0800225](https://openairdocs.org/sdr/CALA0800225.md): Skin · cracked · Mar 17, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > R-1 DOOR CUTOUT LWR AFT CORNER CRACKED APPROX 1.5 INCHES LONG. INSTALLED REPAIR REF SRM 53-10-01 REPAIR 2.
- [SDR CALA0800221](https://openairdocs.org/sdr/CALA0800221.md): Skin · dented · Mar 16, 2008 · N59338 · Boeing 7373T0 · Cargo/Baggage Doors
  > C2 AFT CARGO DOOR, DENT FOUND ON OUTER SKIN, CUT OUT DAMAGE APPROX 2 INCH SQ AT 22 INCH FROM TOP, 31 INCH FROM FWD. INCORPORATED PREVIOUS REPAIR TO FORM ON DOUBLER PER SRM 52-00-01 FIG 201 REPAIR 3. DIP ISSUED TO INSPECT REPAIR PER SRM 52-00-01 REPAIR 3 WITH
- [SDR CALA0800222](https://openairdocs.org/sdr/CALA0800222.md): Door Frame · cracked · Mar 15, 2008 · N59338 · Boeing 7373T0 · Fuselage Main, Structure
  > AFT FRAME WEB IS CRACKED ABOVE UPPER I/B BOLT OF LOWER STOP PAD, FWD CARGO DOOR, AFT FRAME WEB. REPLACED C-1 AFT FRAME PER SRM 51-40-02.
- [SDR CALA0500410](https://openairdocs.org/sdr/CALA0500410.md): Structure · corroded · Nov 16, 2005 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LOWER O/B CHORD CORRODED AT STA 227.8 FROM LBL 6 TO RBL 8. REPAIRED IAW ECRA 5311-01245.
- [SDR CALA0500409](https://openairdocs.org/sdr/CALA0500409.md): Strap · corroded · Nov 16, 2005 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO STRAP ON FRAME CORRODED AT STA 847 ABOVE S25R. THE STRAP ON FRAME WAS REPAIRED IAW ECRA 5311-01244.
- [SDR CALA0500406](https://openairdocs.org/sdr/CALA0500406.md): Gate · corroded · Nov 15, 2005 · N59338 · Boeing 7373T0 · Galley Doors
  > INSPECTION FOUND THE R-1 DOOR LOWER GATE CORRODED AT STOP PINS AND LOWER EDGE, STA 312-328, S18R. A NEW LOWER GATE WAS INSTALLED IAW MM 52-41-61. ADJUSTMENT AND CHECK PERFORMED PER WORK CARD 03-5230-1-8651.
- [SDR CALA0500403](https://openairdocs.org/sdr/CALA0500403.md): Stringer · corroded · Nov 13, 2005 · N59338 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25L CORRODED BETWEEN STA 344 AND 360 AT FORWARD O/B SUPPORT FOR E-2 AVIONICS RACK. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03.
- [SDR CALA0500402](https://openairdocs.org/sdr/CALA0500402.md): Skin · cracked · Nov 13, 2005 · N59338 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1/2" CRACK IN AFT CARGO DOOR INNER SKIN AT LIGHTENING HOLE ABOVE DOOR HANDLE, STA 807-847. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01068.
- [SDR CALA0500401](https://openairdocs.org/sdr/CALA0500401.md): Skin · cracked · Nov 12, 2005 · N59338 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1/2" CRACK AT HOLE CUTOUT IN C-1 INNER DOOR SKIN, STA 440-480, S19R TO S24R. REPAIRED IAW ECRA 5232-01067.
- [SDR CALA0500388](https://openairdocs.org/sdr/CALA0500388.md): Frame · cracked · Nov 7, 2005 · N59338 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK JUST BELOW UPPER HINGE, LOWER GUIDE PLATE AREA IN R-1 DOOR FUSELAGE CUTOUT FRAME, STA 294.5, S11 R TO S14R. THE DOOR FUSELAGE CUTOUT FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0400205](https://openairdocs.org/sdr/CALA0400205.md): Stringer · corroded · Mar 2, 2004 · N59338 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED IN FORWARD CARGO AREA AT STA 480-500B. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0400201](https://openairdocs.org/sdr/CALA0400201.md): Skin · gouged · Mar 2, 2004 · N59338 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND RT UPPER WING L/E SKIN GOUGED BETWEEN NR 5 AND NR 6 SLAT, AT WS 250. REPAIRED IAW SRM 51-70-17.
- [SDR CALA0400200](https://openairdocs.org/sdr/CALA0400200.md): Cargo Track · damaged · Mar 1, 2004 · N59338 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN RAIL LOWER FLANGE DAMAGED BY A SCREW JUST AFT OF STA 867 AND ABOVE STRINGER 27L. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53.
- [SDR CALA0400199](https://openairdocs.org/sdr/CALA0400199.md): Cargo Track · damaged · Mar 1, 2004 · N59338 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN RAIL LOWER FLANGE DAMAGED BY A SCREW BETWEEN STA 747-767 ABOVE STRINGER 29L. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53.
- [SDR CALA011005](https://openairdocs.org/sdr/CALA011005.md): Keelbeam · worn · Nov 16, 2001 · N59338 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND THE RT W/W AFT FAIRING ATTACH HARDWARE HAD WORN INTO RT KEEL BEAM LOWER O/B CHORD AT STA 678-727. REPAIRED IAW ECRA 5310-04218.
- [SDR CALA0101004](https://openairdocs.org/sdr/CALA0101004.md): Stiffener · cracked · Nov 15, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.125 INCH CRACK IN RT WHEEL WELL AFT PANEL T-CHORD AT BS 727. A NEW T-CHORD WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0101003](https://openairdocs.org/sdr/CALA0101003.md): Doubler · cracked · Nov 14, 2001 · N59338 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A THREE INCH CRACK RUNNING PAST STOP DRILL IN C-1 DOOR INTERIOR SKIN DOUBLER. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01637.
- [SDR CALA0101001](https://openairdocs.org/sdr/CALA0101001.md): Fitting · corroded · Nov 13, 2001 · N59338 · Boeing 7373T0 · Fuselage, Stabilizer Attach Fittings
  > INSPECTION FOUND VERTICAL STABILIZER ATTACH FITTING IN FUSELAGE CORRODED AT R/H AFT O/B FORWARD LUG AND AT L/H AFT O/B FORWARD LUG. THE CORROSION WAS REMOVED AND AN OVERSIZE BUSHING WAS INSTALLED AT EACH LOCATION IAW ECRA 5340-01356.
- [SDR CALA0100999](https://openairdocs.org/sdr/CALA0100999.md): Beltframe · corroded · Nov 10, 2001 · N59338 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CORRODED IN AFT BAGGAGE BIN AT STA 927, BL 0. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100995](https://openairdocs.org/sdr/CALA0100995.md): Skin · dented · Nov 7, 2001 · N59338 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AND INTERNAL INTERCOSTALS BROKEN AT STA 807 FROM LBL 10 TO RBL 10. REPAIRED IAW SRM 51-10-02.
- [SDR CALA0100994](https://openairdocs.org/sdr/CALA0100994.md): Web · cracked · Nov 6, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1/4" CRACK IN FORWARD BAGGAGE BIN WEB AT DOOR JAMB, STA 492, S25R. REPAIRED WEB IAW SRM 51-70-13.
- [SDR CALA0100993](https://openairdocs.org/sdr/CALA0100993.md): Floor Support · corroded · Oct 31, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 950, RBL 9-17. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0100992](https://openairdocs.org/sdr/CALA0100992.md): Stiffener · corroded · Oct 31, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD STIFFENER LOWER CORNER CORRODED ON R/H SIDE JUST AFT OF STA 1016, BL 0. A TYPICAL FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA0100991](https://openairdocs.org/sdr/CALA0100991.md): Skin · cracked · Oct 31, 2001 · N59338 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 1/4" CRACK AT 2 EACH RIVETS IN L/H WING #3 SLAT SKIN. REPAIRED SKIN IAW SRM 57-43-01, FIGURE 206.
- [SDR CALA0100988](https://openairdocs.org/sdr/CALA0100988.md): Seat Track · corroded · Oct 30, 2001 · N59338 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN L/H I/B SEAT TRACK CORRODED AT STA 917-923, LBL 15. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0100987](https://openairdocs.org/sdr/CALA0100987.md): Floorbeam · corroded · Oct 30, 2001 · N59338 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AROUND SEVERAL FASTENERS AT STA 294.5, LBL 35-51. A NEW CHORD SECTION WAS INSTALLED IAW SRM 53-10-51, FIGURE 205, SHEETS 1-4.
- [SDR CALA0100986](https://openairdocs.org/sdr/CALA0100986.md): Floorbeam · corroded · Oct 30, 2001 · N59338 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 947, BL 0 TO LBL 6. A REPAIR WAS INSTALLED IAW SRM 53-60-51.
- [SDR CALA0100984](https://openairdocs.org/sdr/CALA0100984.md): Web · cracked · Oct 29, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3" CRACK IN WEB AT FLOOR LINE BELOW R/H EXIT OPENING AT STA 637, S17R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100983](https://openairdocs.org/sdr/CALA0100983.md): Attach Angle · cracked · Oct 29, 2001 · N59338 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1" CRACK IN STRINGER 4L ATTACH ANGLE AT BS 305. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100979](https://openairdocs.org/sdr/CALA0100979.md): Seat Track · corroded · Oct 26, 2001 · N59338 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 370. A REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 202.
- [SDR CALA0100977](https://openairdocs.org/sdr/CALA0100977.md): Mount · corroded · Oct 25, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > L1 DOOR AFT GIRT LATCH MOUNT CORRODED. REMOVED AND REPLACED GIRT MOUNT PER SRM 51-10-02.
- [SDR CALA0100976](https://openairdocs.org/sdr/CALA0100976.md): Mount · corroded · Oct 25, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > L1 DOOR FORWARD GIRT LATCH MOUNT CORRODED. REMOVED AND REPLACED LATCH MOUNT BRACKET PER SRM 51-10-02.
- [SDR CALA0100975](https://openairdocs.org/sdr/CALA0100975.md): Web · cracked · Oct 25, 2001 · N59338 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > WEB CRACKED AT STATION 616 AND STR 17 LEFT BELOW LEFT EXIT OPENING. REMOVED AND REPLACED CRACKED WEB PER SRM 51-10-02.
- [SDR CALA0100974](https://openairdocs.org/sdr/CALA0100974.md): Seat Track · corroded · Oct 25, 2001 · N59338 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BS290 RBL 35. REPLACED SEAT TRACK PER SRM 53-00-52.

Next page: https://openairdocs.org/deregistered/N59338-2013-03-21/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 = 'N59338' AND deregistration_id = 'N59338-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N59338-2013-03-21/reports

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