# Service difficulty reports: N59302, cancelled Apr 15, 2009

A list on [N59302, cancelled Apr 15, 2009](https://openairdocs.org/deregistered/N59302-2009-04-15.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 · 64 reports

- [SDR CALA0700742](https://openairdocs.org/sdr/CALA0700742.md): Skin · cracked · Dec 11, 2007 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND 2 INCH CRACK IN FUSELAGE SKIN BETWEEN RT SIDE BETWEEN STA 747 AND 767 ON STR 19R. REPAIRED PER SRM 53-00-01 REPAIR 31 DETAIL 10.
- [SDR CALA0700346](https://openairdocs.org/sdr/CALA0700346.md): Skin · cracked · Jul 11, 2007 · N59302 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A CRACK AT LIGHTENING HOLE IN THE INNER SKIN OF THE FORWARD CARGO DOOR. THE DOOR SKIN WAS REPAIRED IAW ECRA 5230-01797.
- [SDR CALA0600475](https://openairdocs.org/sdr/CALA0600475.md): Shear Tie · corroded · Nov 14, 2006 · N59302 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 747, LBL 4. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A NEW SHEAR TIE WAS INSTALLED IAW SRM 53-00-07, REPAIR 3, FIGURE 201.
- [SDR CALA0600469](https://openairdocs.org/sdr/CALA0600469.md): Keelbeam · corroded · Nov 12, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LT KEELBEAM CORRODED AT STA 520, S28L. THE KEELBEAM SECTION WAS REPLACED IAW SRM 53-60-12.
- [SDR CALA0600465](https://openairdocs.org/sdr/CALA0600465.md): Frame · cracked · Nov 11, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO CUTOUT AFT FRAME LOWER DOOR STOP AT STA 847, S18R TO S27R. THE FRAME WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0600466](https://openairdocs.org/sdr/CALA0600466.md): Keelbeam · corroded · Nov 10, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND RT KEEL BEAM CORRODED ON INBOARD SIDE JUST AFT OF BULKHEAD AT STA 536. THE KEEL BEAM SECTION WAS REPLACED IAW SRM 53-60-12.
- [SDR CALA0600460](https://openairdocs.org/sdr/CALA0600460.md): Attach Angle · cracked · Nov 10, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN ANGLE THAT ATTACHES STRINGER TO WEB AT STA 360, S14L. THE ANGLE WAS REPLACED IAW ECRA 5311-01277.
- [SDR CALA0600454](https://openairdocs.org/sdr/CALA0600454.md): Frame · corroded · Nov 10, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND LOWER FRAME CORRODED AT STA 227.8, RBL 3 TO LBL 3, S1L TO S1R. A REPAIR WAS INSTALLED IAW ECRA 5311-01275.
- [SDR CALA0600452](https://openairdocs.org/sdr/CALA0600452.md): Stringer · corroded · Nov 9, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R CORRODED AT STA 864. THE STRINGER WAS REPLACED IAW SRM 53-00-03.
- [SDR CALA0600496](https://openairdocs.org/sdr/CALA0600496.md): Skin · corroded · Nov 3, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN PANEL CORRODED AT STA 727 + 4.00 AND CENTERED OVER THE LT KEEL BEAM AT S27L. THE SKIN WAS REPAIRED IAW ECRA 5331-01274.
- [SDR CALA0600449](https://openairdocs.org/sdr/CALA0600449.md): Shear Tie · cracked · Nov 2, 2006 · N59302 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND A.5 INCH CRACK IN LOWER SHEAR TIE FOR FUSELAGE FRAME AT STA 360, S13L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0600444](https://openairdocs.org/sdr/CALA0600444.md): Seat Track · corroded · Oct 30, 2006 · N59302 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 897-927, RBL 45.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52.
- [SDR CALA0600439](https://openairdocs.org/sdr/CALA0600439.md): Attach Fitting · cracked · Oct 29, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE TO BELTFRAME CLIP AT STA 616, S7L TO S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600438](https://openairdocs.org/sdr/CALA0600438.md): Angle · corroded · Oct 29, 2006 · N59302 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 907-1006, LBL 34 TO LBL 60. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0600437](https://openairdocs.org/sdr/CALA0600437.md): Beltframe · cracked · Oct 29, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 616, S7L. REPAIRED IAW SRM 53-00-07.
- [SDR CALA0600436](https://openairdocs.org/sdr/CALA0600436.md): Seat Track · corroded · Oct 29, 2006 · N59302 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 907-938, BL 0. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-02, REPAIR 3.
- [SDR CALA0600430](https://openairdocs.org/sdr/CALA0600430.md): Floorbeam · corroded · Oct 26, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 50 TO RBL 25. DOUBLERS AND A SECTION OF T-CHORD WERE INSTALLED IAW SRM 53-10-51.
- [SDR CALA0600429](https://openairdocs.org/sdr/CALA0600429.md): Seat Track · corroded · Oct 25, 2006 · N59302 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 907-947.5, LBL 24.75. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0600428](https://openairdocs.org/sdr/CALA0600428.md): Frame · cracked · Oct 24, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1/2" CRACK IN MAIN FRAME AT STA 616 JUST BELOW FLOOR, S18R. REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0600427](https://openairdocs.org/sdr/CALA0600427.md): Frame · cracked · Oct 24, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 0.6" CRACK IN MAIN FRAME AT STA 616 JUST BELOW FLOOR, S17L. REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0600424](https://openairdocs.org/sdr/CALA0600424.md): Stringer · corroded · Oct 23, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R IN AFT CARGO COMPARTMENT CORRODED FROM STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-80-03 AND BOEING DRAWING 65-45776.
- [SDR CALA0600419](https://openairdocs.org/sdr/CALA0600419.md): Floorbeam · corroded · Oct 18, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > CORRODED AFT ENTRY FLOORBEAM AT STA 986.5. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0600411](https://openairdocs.org/sdr/CALA0600411.md): Floorbeam · corroded · Oct 16, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM 312 RBL 35. REPAIRED IAW SRM 53-10-51, REPAIR 5, FIG 201.
- [SDR CALA0600280](https://openairdocs.org/sdr/CALA0600280.md): Door Frame · cracked · Jul 30, 2006 · N59302 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1" CRACK IN AFT CARGO DOOR AT PULLEY ATTACHMENT. THE AFT CARGO DOOR FORWARD UPPER AND LOWER CORNER ASSEMBLY (FRAME) WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600279](https://openairdocs.org/sdr/CALA0600279.md): Frame · corroded · Jul 30, 2006 · N59302 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND AFT PIT FORWARD FLOOR FRAME UNDER CAMPLATE CORRODED THROUGH FRAME AT STA 787-807, S2R TO S17R. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR ZN3R543100](https://openairdocs.org/sdr/ZN3R543100.md): Plenum · ruptured · Dec 12, 2005 · N59302 · Boeing 7373TO · APU Core Engine
  > TURBINE PLENUM OF APU RUPTURED AT A PREVIOUSLY REPAIRED WELD SEAM.
- [SDR CALA0500133](https://openairdocs.org/sdr/CALA0500133.md): Skin · corroded · Apr 14, 2005 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED AT NR 3 VHF ANTENNA SUPPORT. INSTALLED CHANNEL PER ECRA 5331-01179.
- [SDR CALA0500084](https://openairdocs.org/sdr/CALA0500084.md): Skin · corroded · Mar 22, 2005 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE FUSELAGE SKIN UNDER NR 3 VHF ANTENNA CORRODED, STA 727D, S29L TO S29R. INSTALLED REPAIR IAW ECRA 5331-01179.
- [SDR CALA0500083](https://openairdocs.org/sdr/CALA0500083.md): Stringer · corroded · Mar 22, 2005 · N59302 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND SKIN BULGING AT STA 360 MINUS 6 INCHES TO 360 WITH CORROSION ON STRINGER 25L. REPAIRED STRINGER IAW ECRA 5311-01219.
- [SDR CALA0500014](https://openairdocs.org/sdr/CALA0500014.md): Skin · cracked · Jan 19, 2005 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN EIGHT INCHES FORWARD OF STA 727E AND BELOW STRINGER 22L. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5330-03410. A DIP WAS ISSUED TO INSPECT PER PART 2 WITHIN 60,000 FLIGHT CYCLES FROM REPAIR INSTALLATION AND TH
- [SDR CALA0500008](https://openairdocs.org/sdr/CALA0500008.md): Skin · cracked · Jan 14, 2005 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN SKIN AFT OF RT WING TO BODY FAIRING, 10 INCHES AFT OF EMERGENCY LIGHT (JUST 2 INCHES FORWARD OF BS 727E AT S23R). INSTALLED SKIN REPAIR IAW ECRA 5330-03409. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT CYCLE
- [SDR CALA0200493](https://openairdocs.org/sdr/CALA0200493.md): Skin · cracked · Oct 11, 2002 · N59302 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND AN 8" CRACK IN R/H WING FIXED L/E SKIN PANEL ABOVE #4 SLAT ACTUATOR. THE SKIN PANEL WAS REMOVED AND REPLACED IAW ECRA 5720-01894.
- [SDR CALA0200488](https://openairdocs.org/sdr/CALA0200488.md): Stringer · corroded · Oct 7, 2002 · N59302 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 23L CORRODED AT STA 375 IN FORWARD CARGO PIT. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A NEW SECTION OF STRINGER WAS SPLICED IN IAW SRM 53-00-03.
- [SDR CALA0200487](https://openairdocs.org/sdr/CALA0200487.md): Floorbeam · cracked · Oct 5, 2002 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CRACKED ON UPPER ANGLE AT STA 328, LBL 12. THE CRACKED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA0200481](https://openairdocs.org/sdr/CALA0200481.md): Floor Support · corroded · Oct 1, 2002 · N59302 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 990 FROM LBL 14 TO LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0200479](https://openairdocs.org/sdr/CALA0200479.md): Seat Track · corroded · Sep 29, 2002 · N59302 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 270 AND 294.5, RBL 43 UNDER G-1 GALLEY. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 AND 51-10-02.
- [SDR CALA0200112](https://openairdocs.org/sdr/CALA0200112.md): Oven · malfunctioned · Feb 28, 2002 · N59302 · Boeing 7373T0 · Buffet/Galleys
  > A STRONG TOXIC ODOR WAS OBSERVED IN THE CABIN WHILE EN ROUTE FROM MSY TO EWR. THE CABIN CREW AND PASSENGERS COMPLAINED OF THE ODOR. THE FLIGHT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THAT A RELAY WITHIN THE AFT GALLEY N
- [SDR CALA0100652](https://openairdocs.org/sdr/CALA0100652.md): Aileron · crushed · Jul 12, 2001 · N59302 · Boeing 7373T0 · Ailerons
  > INSPECTION FOUND LEADING EDGE I/B CORNER OF L/H AILERON CRUSHED. THE AILERON WAS REPAIRED IAW ECRA 5761-01026.
- [SDR CALA0100651](https://openairdocs.org/sdr/CALA0100651.md): Skin · dented · Jul 11, 2001 · N59302 · Boeing 7373T0 · Electrical/Electronic Compartment Doors
  > INSPECTION FOUND EXTERNAL SKIN OF E&E DOOR DENTED. THE E&E DOOR OUTER SKIN WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0100649](https://openairdocs.org/sdr/CALA0100649.md): Light · inoperative · Jul 11, 2001 · N59302 · Boeing 7373T0 · Emergency Lighting
  > THE AFT RIGHT SERVICE DOOR EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-11 AND OPERATION CHECKED GOOD.
- [SDR CALA0100648](https://openairdocs.org/sdr/CALA0100648.md): Floor Support · cracked · Jul 11, 2001 · N59302 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN AFT BAGGAGE BIN FLOOR SUPPORT AT STA 767, RBL 14. A REPAIR WAS INSTALLED IAW SRM 53-00-53.
- [SDR CALA0100634](https://openairdocs.org/sdr/CALA0100634.md): Frame · cracked · Jul 6, 2001 · N59302 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A 1" CRACK IN L-1 WINDOW FRAME AT UPPER O/B CORNER. THE WINDOW FRAME WAS REPAIRED IAW SRM 53-10-01.
- [SDR CALA0100633](https://openairdocs.org/sdr/CALA0100633.md): Skin · cracked · Jul 5, 2001 · N59302 · Boeing 7373T0 · Cargo/Baggage Doors
  > A PERMANENT REPAIR WAS INSTALLED WHERE AN INTERIM REPAIR HAD PREVIOUSLY BEEN DONE FOR 4 EACH CRACKS AT LIGHTENING HOLES IN AFT CARGO DOOR INNER SKIN. THE INTERIM REPAIR HAD BEEN PERFORMED IAW ECRA 5230-01488 AND A DIP WAS ISSUED. THE PERMANENT REPAIR WAS INSTA
- [SDR CALA0100487](https://openairdocs.org/sdr/CALA0100487.md): Skin · cracked · May 21, 2001 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN SKIN OF AFT CUTOUT FOR THE E&E COMPARTMENT COOLING EXHAUST AT STA 373. AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02894.
- [SDR CALA9900073](https://openairdocs.org/sdr/CALA9900073.md): Skin · cracked · Jan 24, 1999 · N59302 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF C-2 AFT CARGO DOOR CUTOUT. REPAIRED IAW ECRA 5330-02763.
- [SDR CALA9900072](https://openairdocs.org/sdr/CALA9900072.md): Battery Pack · discharged · Jan 23, 1999 · N59302 · Boeing 7373T0 · Emergency Lighting
  > THE BATTERY CHARGER ASSEMBLY AND BATTERY FAILED SYSTEM FUNCTIONAL CHECK, PACK M1135, STA 629R (28 VDC PRESENT AT PIN 2 OF PLUG POWER SUPPLY). REMOVED AND REPLACED TWO BATTERY PACKS.
- [SDR CALA9900071](https://openairdocs.org/sdr/CALA9900071.md): Keel Beam · corroded · Jan 22, 1999 · N59302 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM CORRODED AT STA 727, STRINGER 27L. A REPAIR WAS INSTALLED IAW ECRA 5310-03814.
- [SDR CALA9900009](https://openairdocs.org/sdr/CALA9900009.md): Floorbeam · corroded · Jan 13, 1999 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT BEAM HAS SURFACE CORROSION AROUND FASTENER HOLES STA 986.5. INSTALLED NEW FLOORBEAM PER EC/RA 5310-03450.
- [SDR CALA9900059](https://openairdocs.org/sdr/CALA9900059.md): Floorbeam · corroded · Jan 11, 1999 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FORWARD GALLEY CORROSION IN HOLES UPPER AND LOWER SURFACE ON FLOORBEAM STA 328 BL 0 TO R1 Z ANGLE. CUT OUT DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED NEW CHORD PER SRM 53-10-51.
- [SDR CALA9801969](https://openairdocs.org/sdr/CALA9801969.md): Floorbeam · corroded · Oct 17, 1998 · N59302 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT NUTPLATES LOCATED IN E/E COMPARTMENT AT STA 312, RBL 3.5 TO 17. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-70-12, FIGURE 1.

Next page: https://openairdocs.org/deregistered/N59302-2009-04-15/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 = 'N59302' AND deregistration_id = 'N59302-2009-04-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N59302-2009-04-15/reports

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