# Service difficulty reports: N70330, cancelled Mar 21, 2013

A list on [N70330, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N70330-2013-03-21.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 · 59 reports

- [SDR CALA0800268](https://openairdocs.org/sdr/CALA0800268.md): Channel · corroded · Mar 27, 2008 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON Z-CHANNEL UNDER L2 DOOR SILL PLATE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02.
- [SDR CALA0700543](https://openairdocs.org/sdr/CALA0700543.md): Skin · cracked · Sep 27, 2007 · N70330 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK IN RIGHT WING LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW SRM 57-41-01, PAGE 202, FIGURE 201.
- [SDR CALA0700536](https://openairdocs.org/sdr/CALA0700536.md): Bracket · cracked · Sep 24, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN STA 500A VHF ANTENNA MOUNTING BRACKET. A NEW ANTENNA MOUNTING BRACKET WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0700535](https://openairdocs.org/sdr/CALA0700535.md): Stringer Clip · corroded · Sep 24, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND STRINGER TIE IN FORWARD BAGGAGE BIN CORRODED AT STA 540, S26L. THE STRINGER TIE WAS REPAIRED IAW SRM 51-40-02 AND GMM 10-900-01.
- [SDR CALA0700534](https://openairdocs.org/sdr/CALA0700534.md): Stringer · corroded · Sep 24, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26L CORRODED AT STA 540. A REPAIR WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0700533](https://openairdocs.org/sdr/CALA0700533.md): Door Frame · cracked · Sep 23, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A.5 INCH CRACK AT LOWER STOP PAD HOLES OF FORWARD BAG BIN DOOR CUTOUT AFT FRAME. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-20723.
- [SDR CALA0700530](https://openairdocs.org/sdr/CALA0700530.md): Frame · cracked · Sep 23, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FORWARD BAGGAGE BIN FRAME WEB AT STA 500, BL 0. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-70-11.
- [SDR CALA0700529](https://openairdocs.org/sdr/CALA0700529.md): Skin · cracked · Sep 22, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT FUSELAGE SKIN LAP AT STA 880, S25R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31.
- [SDR CALA0700527](https://openairdocs.org/sdr/CALA0700527.md): Skin · cracked · Sep 21, 2007 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727E, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA0600384](https://openairdocs.org/sdr/CALA0600384.md): Skin · cracked · Oct 10, 2006 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK R/S AFT OF WING, 12 INCHES AFT OF EMERGENCY LIGHT. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIG 201.
- [SDR CALA0600377](https://openairdocs.org/sdr/CALA0600377.md): Skin · cracked · Oct 8, 2006 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK RT SIDE AFT OF WING, 12 INCHES AFT OF EMERGENCY LIGHT. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIG 201.
- [SDR CALA0600208](https://openairdocs.org/sdr/CALA0600208.md): Battery Pack · discharged · Jun 12, 2006 · N70330 · Boeing 7373T0 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS AT AFT DOORS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REPLACED.
- [SDR CALA0600007](https://openairdocs.org/sdr/CALA0600007.md): Stiffener · cracked · Jan 13, 2006 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A TWO INCH CRACK IN WING CENTER SECTION VERTICAL STIFFENER AT STA 663.75, RBL 6.15. THE STIFFENER WAS REPAIRED IAW EA 5714-01002. A DIP WAS ISSUED TO ACCOMPLISH A VISUAL INSPECTION OF THE STIFFENER FOR CRACKS EVERY 4500 FLIGHT CYCLES AND TO
- [SDR CALA0600033](https://openairdocs.org/sdr/CALA0600033.md): Skin · cracked · May 8, 2005 · N70330 · Boeing 7373T0 · Cargo/Baggage Doors
  > MAINTENANCE FOUND A CRACK AT LIGHTENING HOLE IN THE LOWER INNER SKIN OF THE FORWARD CARGO DOOR WHILE THE DOOR WAS IN SHOP FOR MAINTENANCE. THE DOOR HAD BEEN REMOVED PREVIOUSLY AT HOU DURING A 4C MAINTENANCE CHECK IN MAY OF 2005. THE DOOR WAS REPAIRED IAW ECR
- [SDR CALA0500135](https://openairdocs.org/sdr/CALA0500135.md): Frame · cracked · Apr 28, 2005 · N70330 · Boeing 7373T0 · Fuselage Main, Frame
  > MAIN CABIN STA 616L FRAME INNER CHORD CRACKED. INSTALLED FRAME PER ECRA 5311-01158.
- [SDR CALA0500127](https://openairdocs.org/sdr/CALA0500127.md): Floorbeam · corroded · Apr 26, 2005 · N70330 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CORRODED AT STA 328, LBL 29. INSTALLED NEW ANGLE PER SRM 53-10-51.
- [SDR CALA0500126](https://openairdocs.org/sdr/CALA0500126.md): Floorbeam · corroded · Apr 26, 2005 · N70330 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CORRODED AT STA 328, LBL 29. INSTALLED NEW ANGLE PER SRM 53-10-51.
- [SDR CALA0300471](https://openairdocs.org/sdr/CALA0300471.md): Skin · cracked · Aug 14, 2003 · N70330 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > MAINTENANCE FOUND A SMALL CRACK IN THE LT HORIZONTAL STABILIZER LOWER SKIN JUST FORWARD OF THE REAR SPAR FORWARD FLANGE, STAB STA 152. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5510-01692. A DIP WAS ISSUED TO PERFORM A DETAILED VISUAL INSPECTION OF THE INTERI
- [SDR CALA0300467](https://openairdocs.org/sdr/CALA0300467.md): Panel · delaminated · Aug 14, 2003 · N70330 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING PANEL UPPER SURFACE DELAMINATED O/B OF MLG. THE PANEL WAS REPAIRED IAW BOEING DRAWING 65-50820-188.
- [SDR CALA0300466](https://openairdocs.org/sdr/CALA0300466.md): Skin · cracked · Aug 13, 2003 · N70330 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND NR 1 SLAT LOWER L/E SKIN CRACKED AT O/B TRACK. THERE WERE FOUR CRACKS MEASURING FROM.125 TO.25 INCH IN LENGTH. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01.
- [SDR CALA0300465](https://openairdocs.org/sdr/CALA0300465.md): Panel · gouged · Aug 13, 2003 · N70330 · Boeing 7373T0 · Rudder, Plate/Skin
  > INSPECTION FOUND RUDDER HINGE COVER PANELS NR 9559 AND 9555 GOUGED. NEW PANELS WERE INSTALLED IAW SRM 51-10-02 AND BOEING DRAWING 65C25973.
- [SDR CALA0300464](https://openairdocs.org/sdr/CALA0300464.md): Skin · cracked · Aug 11, 2003 · N70330 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 4 SLAT ACTUATOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-41-01.
- [SDR CALA0300463](https://openairdocs.org/sdr/CALA0300463.md): Channel · corroded · Aug 11, 2003 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CHANNEL CORRODED ON FORWARD SIDE OF AFT PRESSURE BULKHEAD AT LOWER END, STA 1016, BL 0. THE CHANNEL WAS REPAIRED IAW EA 5310-04045 AND DRAWING 65C28106-1.
- [SDR CALA0300462](https://openairdocs.org/sdr/CALA0300462.md): Skin · cracked · Aug 10, 2003 · N70330 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 0.40 INCH CRACK IN PYLON CUTOUT FOR PANEL NR 5727, NR 1 ENGINE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5430-01230.
- [SDR CALA0300461](https://openairdocs.org/sdr/CALA0300461.md): Floor Panel · cracked · Aug 10, 2003 · N70330 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND A 4 INCH CRACK IN PILOT'S LT SIDE FLOOR PANEL. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300459](https://openairdocs.org/sdr/CALA0300459.md): Attach Angle · cracked · Aug 10, 2003 · N70330 · Boeing 7373T0 · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN ATTACH ANGLE ON HORIZONTAL STABILIZER CENTER SECTION AT UPPER BEAM. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300456](https://openairdocs.org/sdr/CALA0300456.md): Floor Support · cracked · Aug 9, 2003 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5000 INCH CRACK IN CABIN FLOOR SUPPORT BETWEEN BS 380-400, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300088](https://openairdocs.org/sdr/CALA0300088.md): Skin · nicked · Mar 3, 2003 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A NICK IN L/H FUSELAGE SKIN AT STA 235.8, 17.7 INCHES BELOW WL 207.5. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5330-03218.
- [SDR CALA0100535](https://openairdocs.org/sdr/CALA0100535.md): Keelbeam · cracked · May 25, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND A 0.045 INCH CRACK AT HOLE OF KEEL BEAM RT LOWER CHORD, STA 682, RBL 8 (WHEEL WELL AREA). THE CRACKED AREA WAS REMOVED, A FREEZE PLUG AND REPAIR STRAP WAS INSTALLED IAW ECRA 5310-04144.
- [SDR CALA0100485](https://openairdocs.org/sdr/CALA0100485.md): Web · cracked · May 20, 2001 · N70330 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 0.3 INCH CRACK IN C-2 DOOR AT LIGHTENING HOLE LOCATED AT ACCESS TO SPRING SUPPORT FITTING. THE CRACKED AREA WAS TRIMMED AND DRESSED UP AND A DOUBLER WEB REPAIR WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0100461](https://openairdocs.org/sdr/CALA0100461.md): Skin · cracked · May 16, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AND INTERIOR SUPPORT FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E, BL 0. REPAIRED IAW SRM 53-00-01.
- [SDR CALA0100460](https://openairdocs.org/sdr/CALA0100460.md): Skin · damaged · May 16, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A SMALL CREASE IN FUSELAGE SKIN AT STA 1042, S13L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202 AND 51-70.
- [SDR CALA0100459](https://openairdocs.org/sdr/CALA0100459.md): Skin · dented · May 16, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1008, S16L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.
- [SDR CALA0100458](https://openairdocs.org/sdr/CALA0100458.md): Spar · cracked · May 15, 2001 · N70330 · Boeing 7373T0 · Wing Spar
  > INSPECTION FOUND A 0.1 INCH CRACK IN RT REAR SPAR UPPER CHORD AT RT MLG BEAM O/B END AFT SPAR FITTING ATTACH AREA. THE CRACK WAS REPAIRED IAW ECRA 5743-01033. A DIP WAS ISSUED TO REINSPECT THE AREA AT 3,000 FLIGHT CYCLE INTERVALS.
- [SDR CALA0100455](https://openairdocs.org/sdr/CALA0100455.md): Stringer · gouged · May 12, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 14R GOUGED AT STA 600. A NEW STRINGER SECTION WAS INSTALLED IAW SRM 53-00-03, PAGE 201.
- [SDR CALA0100449](https://openairdocs.org/sdr/CALA0100449.md): Seat Track · corroded · May 7, 2001 · N70330 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 887-947.5. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0100448](https://openairdocs.org/sdr/CALA0100448.md): Angle · corroded · May 7, 2001 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-1 DOOR ENTRYWAY Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-2.
- [SDR CALA0100443](https://openairdocs.org/sdr/CALA0100443.md): Floorbeam · corroded · May 4, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 312, LBL 12-RBL 12. THE MAJORITY OF CORROSION WAS BURNISHED OUT. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-1 AT ONE LOCATION FOUND OUT OF LIMITS.
- [SDR CALA0100121](https://openairdocs.org/sdr/CALA0100121.md): Bulkhead · cracked · Feb 15, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND TWO CRACKS ON FLOOR STRUCTURE WEB AT LT AND RT W/L 195, ONE CRACK ON CENTER WEB AT W/L 200, LBL 5.7 AND ONE CRACK ON CENTER WEB AT W/L 201, RBL 5.7 DURING 737 FUS-BS 178 BULKHEAD INSPECTION. THE CRACKS WERE.5 INCH IN LENGTH. REPAIRS WERE
- [SDR CALA0100114](https://openairdocs.org/sdr/CALA0100114.md): Skin · cracked · Feb 10, 2001 · N70330 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN AFT SKIN CUTOUT FOR THE E&E COMPARTMENT COOLING EXHAUST. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894.
- [SDR CALA9900555](https://openairdocs.org/sdr/CALA9900555.md): Skin · cracked · May 17, 1999 · N70330 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN NR 2 ENGINE PYLON SKIN AT PANEL NR 5824 AND A.5 INCH CRACK WAS FOUND IN PANEL NR 5828. REPAIRS WERE INSTALLED IAW ECRA 5430-01230.
- [SDR CALA9700776](https://openairdocs.org/sdr/CALA9700776.md): Floorbeam · corroded · May 16, 1997 · N70330 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT STA 986.5. THE CORRODED AREA WAS CUT OUT AND A T-SECTION WAS INSTALLED IAW ECRA 5310-03450.
- [SDR CALA9700786](https://openairdocs.org/sdr/CALA9700786.md): Angle · cracked · May 14, 1997 · N70330 · Boeing 7373T0 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN NR 3 FLAP FAIRING WING TRAILING EDGE ATTACH ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA9700784](https://openairdocs.org/sdr/CALA9700784.md): Support · corroded · May 9, 1997 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 950, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9700775](https://openairdocs.org/sdr/CALA9700775.md): Strap · corroded · May 9, 1997 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT AFT LAV STRAP CORRODED AT BS 1006 TO 1016, LBL 3. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2.
- [SDR CALA9700783](https://openairdocs.org/sdr/CALA9700783.md): Support · corroded · May 8, 1997 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 299, RBL 20. A REPAIR WAS INSTALLED IAW ECRA 5310-03477.
- [SDR CALA9700781](https://openairdocs.org/sdr/CALA9700781.md): Floorbeam · corroded · May 8, 1997 · N70330 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344 LBL 31.6 TO L-1 DOOR AND RBL 30 TO LBL 10. THE CORRODED AREAS WERE REMOVED, REPAIRS WERE INSTALLED IAW SRM 53-10-51 AND ECRA 5310-03480.
- [SDR CALA9700780](https://openairdocs.org/sdr/CALA9700780.md): Floorbeam · corroded · May 8, 1997 · N70330 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 294.5, RBL 0. A NEW FLOORBEAM SECTION WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA9700779](https://openairdocs.org/sdr/CALA9700779.md): Support · corroded · May 8, 1997 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED BETWEEN STA 294.5 AND 312, RBL 15 AND RBL 30. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ECRA 5310-03477 AND SRM 51-10-02.
- [SDR CALA9700785](https://openairdocs.org/sdr/CALA9700785.md): Support · corroded · May 7, 1997 · N70330 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT AFT LAV FLOOR SUPPORT CORRODED AT BS 986 TO 990, RBL 10. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10-00.

Next page: https://openairdocs.org/deregistered/N70330-2013-03-21/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 = 'N70330' AND deregistration_id = 'N70330-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N70330-2013-03-21/reports

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