# Service difficulty reports: N330DL, cancelled Mar 13, 2007

A list on [N330DL, cancelled Mar 13, 2007](https://openairdocs.org/deregistered/N330DL-2007-03-13.md).

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

- [SDR DL73S060013](https://openairdocs.org/sdr/DL73S060013.md): Skin · cracked · Dec 13, 2005 · N330DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS 3 INCH LONG LOCATED JUST AFT OF BS 727B, JUST BELOW S-18L. INSTALLED A DOUBLER IAW ER/A 452077-14AD.
- [SDR DL73S050097](https://openairdocs.org/sdr/DL73S050097.md): Frame · cracked · Feb 8, 2005 · N330DL · Boeing 737232 · Fuselage Main, Frame
  > A FASTENER HOLE COMMON TO THE OUTER CHORD OF THE AFT FRAME OF THE L2 DOOR CUTOUT (FS 992, BETWEEN STRINGERS 7L & 8L) WAS FOUND CRACKED. THE HOLE WAS OVERSIZED AND AN INSURANCE CUT MADE TO REMOVE THE CRACK. THE OVERSIZED HOLE WAS REPAIRED WITH AN ALUMINUM BUS
- [SDR DL73S031040](https://openairdocs.org/sdr/DL73S031040.md): Skin Panel · cracked · Nov 21, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF 03-058543-03, ME-01 EXISTING REPAIRS AND NEW CRACK DAMAGE WERE NOTED ON THE KEEL BEAM LOWER SKIN PANEL. THE SUBJECT SKIN PANEL WAS REPLACED PER INSTRUCTIONS CONTAINED IN ERA 385772-14.
- [SDR DL73S031039](https://openairdocs.org/sdr/DL73S031039.md): Attach Fitting · corroded · Nov 21, 2003 · N330DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > DURING ACCOMPLISHMENT OF 03-069697-03 NUMEROUS ATTACHMENT LUGS REQUIRED MACHINING BEYOND THE LIMITS PROVIDED, IN ORDER TO REMOVE ALL CORROSION DAMAGE FOUND. LUGS WERE REWORKED PER INSTRUCTIONS CONTAINED IN ERA 385802-14AD.
- [SDR DL73S031033](https://openairdocs.org/sdr/DL73S031033.md): Floorbeam · corroded · Nov 20, 2003 · N330DL · Boeing 737232 · Fuselage Main, Floor Beam
  > DURING MODIFICATION OF THE BL 24 FLOORBEAMS PER EO 03-056673-03AD ADDITIONAL WORK WAS REQUIRED DUE TO ADDITIONAL DAMAGE INCURRED. ERA 385831-14AD IMPLEMENTS THE LBL 24 BEAM MOD, PROVIDES NEW REPAIRS FOR THE BEAM WEBS AND ADDRESSES INCURRED DAMAGE.
- [SDR DL73S031028](https://openairdocs.org/sdr/DL73S031028.md): Fitting · corroded · Nov 19, 2003 · N330DL · Boeing 737232 · Vertical Stabilizer, Attach Fittings
  > CORROSION DAMAGE WAS FOUND ON THE VERTICAL STAB NR 2 FIN LUG AND THE NR 11 BODY CLEVIS LUG. CORROSION WAS REMOVED AND REWORKED PER ERA 385810-14.
- [SDR DL73S031036](https://openairdocs.org/sdr/DL73S031036.md): Skin · damaged · Nov 17, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DAMAGED AROUND 2 NUT PLATE HOLES USED FOR ATTACHMENT OF A WING TO FUSELAGE FAIRING PANEL AT FS 760 BETWEEN STRINGERS 19R & 20R. THE DAMAGED HOLES WERE REMOVED WITH 1.5 X 1 INCH LOCAL CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGL
- [SDR DL73S031035](https://openairdocs.org/sdr/DL73S031035.md): Skin · gouged · Nov 17, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED NEAR FS 178 AND STRINGER 24R. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 087582-14, REV A.
- [SDR DL73S031025](https://openairdocs.org/sdr/DL73S031025.md): Skin · dented · Nov 17, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A DENT WAS NOTED IN THE FUSELAGE SKIN AT BS 380, BETWEEN S17L AND S18-L. THE DENT WAS CUT OUT AND REPAIRED PER ERA 385827-14.
- [SDR DL73S031010](https://openairdocs.org/sdr/DL73S031010.md): Floorbeam · cracked · Nov 12, 2003 · N330DL · Boeing 737232 · Fuselage Main, Floor Beam
  > THE FS 520 FLOORBEAM WAS FOUND WITH 1 INCH TO 2 INCH CRACKS NEAR THE UPPER CAP FLANGE AT RBL & LBL 24 & 45. THE CRACKS WERE TYPICAL OF BAC S/B 737-53-1120. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL CRACKS. A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION
- [SDR DL73S030975](https://openairdocs.org/sdr/DL73S030975.md): Stop Fitting · damaged · Oct 29, 2003 · N330DL · Boeing 737232 · Cargo/Baggage Doors
  > DURING ACCOMPLISHMENT OF EO 3-059252-3AD, OPN 0301, (S/B 737-52A1100), A 65-46861-0) FITTING WAS FOUND. EO INSTRUCTIONS REQUIRE ENGINEERING EVALUATION. EVALUATION FOUND THAT FITTING REQUIRED REPLACEMENT PER S/B 737-52-1065. FITTING REPLACED PER S/B 737-52-1
- [SDR DL73K030896](https://openairdocs.org/sdr/DL73K030896.md): Frame · cracked · Oct 2, 2003 · N330DL · Boeing 737232 · Cargo/Baggage Doors
  > THE LOWER FORWARD FRAME OF THE C1 DOOR HAD A TIME-LIMITED REPAIR PREVIOUSLY INSTALLED AND NEEDED PERMANENT REPAIR INSTRUCTIONS. PERMANENT REPAIR ISSUED VIA ERA 377407-14AD, REV A.
- [SDR DL73K011340](https://openairdocs.org/sdr/DL73K011340.md): Keelbeam · cracked · Aug 14, 2001 · N330DL · Boeing 737232 · Fuselage Main, Keel
  > THE LT STRINGER 18A SHEAR BEAM AT FS 727 WAS FOUND WITH A 1 INCH CRACK EMANATING FROM THE EDGE OF THE WEB. THE CRACK IS TYPICAL OF THOSE SHOWN IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED
- [SDR DL73K010377](https://openairdocs.org/sdr/DL73K010377.md): Keelbeam · cracked · Mar 6, 2001 · N330DL · Boeing 737232 · Fuselage Main, Keel
  > THE RT STRINGER 18A SHEAR BEAM WAS FOUND WITH A WEB CRACK AT FS 727. THE CRACK IS TYPICAL OF THOSE FOUND IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A STEEL REPAIR CHANNEL PER ER/
- [SDR DL73K002530](https://openairdocs.org/sdr/DL73K002530.md): Relay · failed · Dec 29, 2000 · N330DL · Boeing 737232 · Fuel Boost Pump
  > DURING CLIMB RIGHT CENTER LOW PRESSURE LIGHT ILLUMINATED. CB POPPED RETURNED TO EWR. - REPLACED CONTROL RELAY FOR RT CENTER FUEL BOOST PUMP
- [SDR DL73K001620](https://openairdocs.org/sdr/DL73K001620.md): Light · inoperative · Aug 21, 2000 · N330DL · Boeing 737232 · Emergency Lighting
  > ON LAYOVER, EMERGENCY LIGHT INOP AT ROW 10 DEF. REPLACED LIGHT ASSY, CKS GOOD.
- [SDR DL73K000674](https://openairdocs.org/sdr/DL73K000674.md): Seat · cracked · Apr 8, 2000 · N330DL · Boeing 737232 · Passenger Compartment Equipment
  > SEAT ROW 3 DEF LOOSE ON MOUNTS LIKE A ROCKING CHAIR. FOUND SEAT FRAME CRACKED. REPLACED SEAT ASSEMBLY.
- [SDR DL73K990542](https://openairdocs.org/sdr/DL73K990542.md): Frame · cracked · Mar 11, 1999 · N330DL · Boeing 737232 · Fuselage Main, Frame
  > THE AFT DOOR JAMB FRAME OF THE R1 DOOR OPENING WAS FOUND WITH A 3 INCH LONG CRACK UNDER UPPER DOOR STOP FITTING. THE CRACKED FRAME WAS REPAIRED PER THE REQUIREMENTS OF B737 SRM 53-10-4, FIG 1 AND DOCUMENTED PER ER/A 366934-14AD.
- [SDR DL73S981794](https://openairdocs.org/sdr/DL73S981794.md): Actuator · failed · Aug 30, 1998 · N330DL · Boeing 737232 · Stabilizer Actuator
  > RUNAWAY STAB TRIM ON SHORT FINAL. GO-AROUND MADE. REPLACED STAB TRIM ACTUATOR.
- [SDR DL73S980538](https://openairdocs.org/sdr/DL73S980538.md): Skin · gouged · Mar 9, 1998 · N330DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SEVERAL GOUGES AND NICKS WERE FOUND IN THE EDGE OF THE SKIN O THE AFT SIDE OF THE C1 DOOR CUTOUT AT APPROX FS 489, BETWEEN S21R AND S23R. REPAIRED PER ERA 331462-14.
- [SDR DL73S980537](https://openairdocs.org/sdr/DL73S980537.md): Intercostal · cracked · Mar 9, 1998 · N330DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION PER SI 3-55852-12, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT 3 LOCATIONS S8A, 10A, AND 11A. REPAIRED PER ERA 331432-14AD.
- [SDR DL73S960651](https://openairdocs.org/sdr/DL73S960651.md): Blkhd Web · cracked · Mar 14, 1996 · N330DL · Boeing 737232 · Fuselage Main, Bulkhead
  > THE BS 178 BULKHEAD WEB WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN A 1.45 INCH LEFT AND RIGHT BY 1.2 INCH UP AND DOWN CUTOUT ON THE LT SIDE AND A 1.5 INCH LEFT AND RIGHT BY 5.1 INCH UP AND DOWN CUTOUT
- [SDR DL73S953838](https://openairdocs.org/sdr/DL73S953838.md): Cowl · dented · Sep 8, 1995 · N330DL · Boeing 737232 · Engine Cowling System
  > DURING SHOP VISIT, ENGINE NOSE COWL ASSEMBLY WAS RESTORED PER CMM 65-85378. OUTER SKIN DENTED AT 5:30 POSITION. REPAIRED PER SRM 51-40-2.

## 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 = 'N330DL' AND deregistration_id = 'N330DL-2007-03-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N330DL-2007-03-13/reports

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