# Service difficulty reports: N76355, cancelled Aug 11, 2011

A list on [N76355, cancelled Aug 11, 2011](https://openairdocs.org/deregistered/N76355-2011-08-11.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 · 72 reports

- [SDR CALA0800918](https://openairdocs.org/sdr/CALA0800918.md): Support · cracked · Sep 23, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > PARTITION SUPPORT CRACKED AFT OF STA 1016. REMOVED AND REPLACED PARTITION SUPPORT PER 737-300 SRM 51-10-02.
- [SDR CALA0800923](https://openairdocs.org/sdr/CALA0800923.md): Keelbeam · corroded · Sep 22, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Keel
  > KEEL BEAM FOUND WITH CORROSION IN FORWARD CARGO AT BODY STATION 500D+8" TO 500D+12.5" AT LBL 6.5". REPAIRED KEEL BEAM PER B737 SRM 53-60-12, REINSTALLED REMOVED COMPONENTS, PERFORMED LEAK CHECK, NO LEAKS PRESENT AT THIS TIME IAW B737-300 MM 36-19-15.
- [SDR CALA0800907](https://openairdocs.org/sdr/CALA0800907.md): Angle · corroded · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION ON TRANSITION ANGLE AT STATION 767 STR 24R. REMOVED BAD SECTION OF TRANSITION ANGLE, FABRICATED NEW ANGLE, ALODINED, PRIMED AND INSTALLED NEW SECTION OF ANGLE PER SRM 51-40-02, SRM 51-40-05, AMM51-20-00.
- [SDR CALA0800902](https://openairdocs.org/sdr/CALA0800902.md): Bulkhead · damaged · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WEB FROM FLOOR LEVEL TO Y-CORD FROM APPROXIMATELY LBL 6 TO APPROXIMATELY LBL 20 HAS OVERHEAT DAMAGE. REMOVED AFT PRESSURE BULKHEAD WEB FROM CENTER RING TO Y-CHORD AND REPLACED BULKHEAD WEB (P/N-65-46568Y524) AND DOUBLER (P/N-65-46568-696
- [SDR CALA0800885](https://openairdocs.org/sdr/CALA0800885.md): Stiffener · damaged · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > STIFFENER ON AFT PRESS BULKHEAD JUST O/B OF APU BLEED DUCT HAS OVERHEAT DAMAGE FROM FLOOR LEVEL DOWN TO Y-CORD. REMOVED STIFFENER FROM AFT PRESSURE BULKHEAD JUST OUTBOARD OF APU BLEED DUCT AND INSTALLED NEW STIFFENER PER 13-737-300 SRM 51-40-02.
- [SDR CALA0800884](https://openairdocs.org/sdr/CALA0800884.md): Stiffener · damaged · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > STIFFENER ON AFT PRESS BULKHEAD JUST I/B OF APU BLEED DUCT HAS OVERHEAT DAMAGE FROM FLOOR LEVEL DOWN TO Y-CORD. REMOVED STIFFENER ON AFT PRESSURE BULKHEAD JUST INBOARD OF APU BLEED DUCT AND INSTALLED NEW STIFFENER PER SRM 51-40-02.
- [SDR CALA0800883](https://openairdocs.org/sdr/CALA0800883.md): Intercostal · overheated · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT LBL 18.32 FROM 1016 TO AFT PRESS BULKHEAD HAS OVERHEAT DAMAGE. REMOVED INTERCOSTAL IAW B737 SRM 51-40-02. FABRICATED INTERCOSTAL IAW BAC DWG 65C32677. INSTALLED INTERCOSTAL IAW B737 SRM 51-40-02 AT LBL 18.32 AFT PRESS BULKHEAD.
- [SDR CALA0800882](https://openairdocs.org/sdr/CALA0800882.md): Stiffener · damaged · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > Z-ANGLE STIFFENER FROM LBL 3.54 TO LBL 18.32 ADJACENT TO AFT PRESSURE BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED Z-ANGLE STIFFENER IAW SRM 51-A01-02. FABRICATED NEW STIFFENER IAW DWG 65-46812 INSTALLED NEW Z-ANGLE STIFF IAW SRM 51-40-02 AT LBL 3.54-LBL 18
- [SDR CALA0800881](https://openairdocs.org/sdr/CALA0800881.md): Stiffener · overheated · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > Z-ANGLE STIFFENER FROM LBL 18.32 TO 27.95 ADJACENT TO AFT PRESSURE BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED Z-ANGLE STIFFENER IAW SRM51-40-02. FABRICATED NEW STIFFENER IAW BAC DWG 65-46812, INSTALLED NEW Z-ANGLE STIFFENER AT LBL 18-32-27.95 AT AFT PRESSU
- [SDR CALA0800880](https://openairdocs.org/sdr/CALA0800880.md): Intercostal · overheated · Sep 16, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT LBL 3.54 FROM BS 1016 TO AFT PRESS BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02. FABRICATED NEW INTERCOSTAL IAW DWG 65-46812. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02 AT LBL 3.54 AFT PRESS BULKHEAD.
- [SDR CALA0800870](https://openairdocs.org/sdr/CALA0800870.md): Spar · corroded · Sep 5, 2008 · N76355 · Boeing 7373T0 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER HAS CORROSION AT FIN STATION 163.90 - 191.50 LEFT-SIDE AT REAR SPAR. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER EC/RA 5530-01510.
- [SDR CALA0800869](https://openairdocs.org/sdr/CALA0800869.md): Frame · cracked · Sep 5, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Frame
  > BODY STATION 303.9 FRAME WEB P/N 65-17684-107 CRACKED AT S16L. BODY STATION 303.9 FRAME WEB REPLACED PER EC/RA 5310-04826.
- [SDR CALA0800868](https://openairdocs.org/sdr/CALA0800868.md): Frame · cracked · Sep 5, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Frame
  > CRACK ON STIFFENER WHERE LOWER CASTING FOR L-1 DOORSTOP MOUNTS TO FRAME AT BODY STATION 303.9 AFT OF STRINGER 16 AT DOOR CUTOUT. REPAIRED FRAME AT BODY STATION 303.9 AND S16L PER EC/RA 5310-04826.
- [SDR CALA0800867](https://openairdocs.org/sdr/CALA0800867.md): Skin · cracked · Sep 5, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > R1 DOOR CUTOUT CRACKED AT LOWER AFT CORNER OF CUTOUT. CUT OUT DAMAGED AREA AND REPAIRED SAME PER SRM 53-10-01 REPAIR 2.
- [SDR CALA0800866](https://openairdocs.org/sdr/CALA0800866.md): Skin · cracked · Sep 5, 2008 · N76355 · Boeing 7373T0 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR SKIN FOUND CRACKED UNDER DOOR LINER AT EDGE OF LIGHTENING HOLE 21" FROM TOP 21.5" FROM FORWARD EDGE. REMOVED CRACK AND REPAIRED FORWARD CARGO DOOR INNER SKIN AT LIGHTENING HOLE 21" FROM TOP AND 21.5" FROM FORWARD EDGE PER SRM 52-30-01 AND S
- [SDR CALA0800865](https://openairdocs.org/sdr/CALA0800865.md): Intercostal · cracked · Sep 5, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT INBOARD AFT FLANGE LOCATED AT BODY STATION 303.9 AND S16L. REPLACED INTERCOSTAL AT BODY STATION 303.9 AND S16L PER EC/RA 5310-04826.
- [SDR CALA0800863](https://openairdocs.org/sdr/CALA0800863.md): Angle · corroded · Sep 5, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CORROSION ON TRANSITION ANGLE AT STATION 727E S-24R. REMOVED BAD TRANSTION ANGLE, FABRICATED NEW SECTION, ALODINED, PRIMED AND INSTALLED ANGLE PER SRM 51-40-02, SRM 51-40-05 AND AMM 51-20-00.
- [SDR CALA0800859](https://openairdocs.org/sdr/CALA0800859.md): Intercostal · corroded · Sep 4, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FLOORBEAMS BS 328 AND 344 HAS CORROSION AT BL15R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FLOORBEAMS PER SRM 51-40-02.
- [SDR CALA0800850](https://openairdocs.org/sdr/CALA0800850.md): Floorbeam · corroded · Sep 4, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT BODY STATION 270 FROM LBL 10 - RBL 10 LOCATED AT AFT SIDE OF NLG DOWNLOCK VIEWER PANEL. REPAIRED CORRODED FLOORBEAM AT BODYSTATION 270 FROM LBL 10 - RBL 10 LOCATED AT AFT SIDE OF NLG DOWNLOCK VIEWER PANEL PER CAL EC/RA5320-01701.
- [SDR CALA0800849](https://openairdocs.org/sdr/CALA0800849.md): Floor Support · corroded · Sep 4, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > G2 GALLEY RIGHT FORWARD FLOOR MOUNT HAS CORROSION. REMOVED MOUNT AND REPLACED THE MOUNT WITH NEW PART IAW SRM 51-40-02.
- [SDR CALA0800848](https://openairdocs.org/sdr/CALA0800848.md): Door Frame · cracked · Sep 4, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Structure
  > FORWARD CARGO DOOR FRAME CRACKED. REMOVED CRACKED DOOR FRAME AND REPLACED SAME WITH NEW DOOR FRAME IAW SRM 51-40-02.
- [SDR CALA0800800](https://openairdocs.org/sdr/CALA0800800.md): Angle · corroded · Aug 21, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > Z-ANGLE AT L1 DOOR HAS CORROSION. REMOVED CORRODED Z-ANGLE AT L1 DOOR AND INSTALLED NEW Z-ANGLE IAW B737 SRM 51-40-02.
- [SDR CALA0800801](https://openairdocs.org/sdr/CALA0800801.md): Frame · cracked · Aug 19, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Frame
  > BODYSTATION 380 FRAME CRACK BETWEEN S20R AND 21R. REPAIRED FRAME AT BODYSTATION 380 IAW B737 SRM 51-70-11.
- [SDR CALA0800797](https://openairdocs.org/sdr/CALA0800797.md): Failsafe · cracked · Aug 19, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Frame
  > FRAME AT BODY STATION 380 BETWEEN S19R AND S20R APPEARS WAVY AT OLD REPAIR. EVALUATE AND REPAIR IF REQUIRED. REMOVED DAMAGED FAILSAFE AND REPAIRED IAW B737 SRM 51-70-11.
- [SDR CALA0800791](https://openairdocs.org/sdr/CALA0800791.md): Skin · cracked · Aug 13, 2008 · N76355 · Boeing 7373T0 · Cargo/Baggage Doors
  > CRACK AT FORWARD CARGO DOOR HANDLE 22.25 INCHES FROM LOWER EDGE AND 17 INCHES FROM AFT EDGE. REMOVED FASTENER, VERIFIED CRACK CONTAINED AT FASTENER HOLE. REPAIRED DAMAGE PER 737-300 SRM 52-00-01 FIG 201.
- [SDR CALA0800790](https://openairdocs.org/sdr/CALA0800790.md): Stringer Clip · cracked · Aug 13, 2008 · N76355 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > STRINGER CLIP AT STATION 727D S23L CRACKED. REMOVED AND REINSTALLED STRINGER CLIP AT STATION 727D S23L PER B737-300 SRM 51-40-02.
- [SDR CALA0800789](https://openairdocs.org/sdr/CALA0800789.md): Seat Track · corroded · Aug 13, 2008 · N76355 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBOARD SEAT TRACK HAS CORROSION FROM FS 328-344. REMOVED SEAT TRACK PER B737 SRM 51-40-02, FABRICATED SEAT TRACK SECTION PER B737 SRM 53-00-52, ALODINED AND PRIMED SEAT TRACK PER B737 SRM 51-20-01, INSTALLED SEAT TRACK PER B737 SRM 51-40-02.
- [SDR CALA0800776](https://openairdocs.org/sdr/CALA0800776.md): Structure · deformed · Aug 6, 2008 · N76355 · Boeing 7373T0 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD MID FLAP DAMAGED ON TRAILING EDGE. REPAIRED DAMAGED AREA RT WING O/B MID FLAP TRAILING EDGE WEDGE REF BOAC 737-300 SRM 51-70-10.
- [SDR CALA0800775](https://openairdocs.org/sdr/CALA0800775.md): Channel · corroded · Aug 6, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT CHANNEL FOR NOSE LANDING GEAR VIEWER PANEL. REMOVED AND REPLACED SUPPORT CHANNEL WITH NEW CHANNEL AND REMOVED AND REINSTALLED UPPER VIEW TUBE PER BOEING DWG 65-45833 B737-300 SRM 51-40-02 AND B737-300 AMM 56-41-31.
- [SDR CALA0800770](https://openairdocs.org/sdr/CALA0800770.md): Intercostal · cracked · Aug 4, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FOUND CRACKED AT FORWARD END BELOW TRANSITION ANGLE AT BODY STATION BS 500 STR 26L. REMOVED CRACKED ANGLE INTERCOSTAL BS 500 STR 26L. DRILLED NEW ANGLE FOR INSTALL IAW B737 SRM 51-40-02, INSTALLED NEW INTERCOSTAL AT STATION 500 STR 26L IAW B737 S
- [SDR CALA0800779](https://openairdocs.org/sdr/CALA0800779.md): Skin · cracked · Jul 28, 2008 · N76355 · Boeing 7373T0 · Cargo/Baggage Doors
  > AFT CARGO DOOR FOUND WITH CRACK APPROX 2.5 INCH ABOVE AFT EDGE OF EXTERNAL HANDLE. REMOVED EXISTING REPAIR DOUBLER PER SRM 51-40-02 FROM AFT CARGO DOOR, FABRICATED NEW REPAIR DOUBLER PER SRM 52-00-01, ALODINED AND PRIMED REPAIR DOUBLER AND BASE SKIN PER SRM 5
- [SDR CALA0800778](https://openairdocs.org/sdr/CALA0800778.md): Angle · corroded · Jul 28, 2008 · N76355 · Boeing 7373T0 · Service Doors
  > R2 DOOR Z-ANGLE CORRODED AND STRAP AFT OF Z=ANGLE IS CORRODED. REMOVED CORRODED R2 Z-ANGLE AND STRAP IAW B737 SRM 51-40-02. CLEANED CORROSION FROM STRAP, FOUND TO BE WITHIN LIMITS PER B737 SRM 51-10-02. LOCATED AND DRILLED NEW Z-ANGLE PER B737 SRM 51-40-05.
- [SDR CALA0800409](https://openairdocs.org/sdr/CALA0800409.md): Intercostal · corroded · May 4, 2008 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STATION 840-855 S-25-R IS CORRODED (LEVEL 2 CORROSION). REPLACED INTERCOSTAL AT STATION 840-855 S-25-R IAW SRM 51-30-01.
- [SDR CALA0700692](https://openairdocs.org/sdr/CALA0700692.md): Skin · cracked · Nov 19, 2007 · N76355 · Boeing 7373T0 · Cargo/Baggage Doors
  > THE RAMP FOUND A 3.5 INCH CRACK IN AFT CARGO DOOR SKIN ABOVE FORWARD DOOR CUTOUT. DOUBLERS WERE INSTALLED IAW ECRA 5232-01096. A DIP WAS INITIATED TO ACCOMPLISH A PERMANENT REPAIR WITHIN SIX MONTHS.
- [SDR CALA0700380](https://openairdocs.org/sdr/CALA0700380.md): Skin · corroded · Jul 8, 2007 · N76355 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING SKIN CORRODED FORWARD OF NR 3 SPOILER, I/B HINGE POINTS, APPROX WS 311.37. REPAIRED IAW ECRA 5720-02022.
- [SDR CALA0700379](https://openairdocs.org/sdr/CALA0700379.md): Skin · corroded · Jul 8, 2007 · N76355 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING SKIN CORRODED ON TOP SURFACE AT APPROX WS 175 JUST FORWARD OF TRAPEZOIDAL PANEL NEAR CENTER LINE. LOCATED ABOUT 17 FASTENERS I/B OF O/B TIP OF TRAPEZOIDAL PANEL FORWARD OF NR 4 SPOILER. REPAIRED IAW ECRA 5720-02022.
- [SDR CALA0700217](https://openairdocs.org/sdr/CALA0700217.md): Wire Harness · unknown · Apr 25, 2007 · N76355 · Boeing 7373T0 · Light System Wiring
  > FOUND EMERGENCY LIGHT ON SEAT 21C INOP. REPAIRED IAW AMM 33-51-81.
- [SDR CALA0700216](https://openairdocs.org/sdr/CALA0700216.md): Light · inoperative · Apr 25, 2007 · N76355 · Boeing 7373T0 · Emergency Lighting
  > FOUND EMERGENCY LIGHT ON SEAT 12C INOP. REPAIRED IAW AMM 33-51-81.
- [SDR CALA0500211](https://openairdocs.org/sdr/CALA0500211.md): Skin · cracked · Jul 3, 2005 · N76355 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND 1.625 INCH CRACK IN FUSELAGE SKIN AT STA 727E, S22R TO S23R. SKIN REPAIRED IAW ECRA 5330-03459.
- [SDR CALA0500177](https://openairdocs.org/sdr/CALA0500177.md): Actuator · inoperative · May 29, 2005 · N76355 · Boeing 7373T0 · Landing Gear Actuator
  > THE LT MLG GREEN LIGHT DID NOT ILLUMINATE FOR SEVERAL MINUTES WHEN GEAR WAS EXTENDED ON APPROACH INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. WHEN MAINTENANCE PERFORMED A GEAR SWING THE LT MAIN GEAR DID NOT EXTEND, BUT MANUAL EXTENSION WAS GOOD. THE LT ML
- [SDR CALA0400731](https://openairdocs.org/sdr/CALA0400731.md): Skin · cracked · Oct 29, 2004 · N76355 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727D AND 727E AT S22L. REPAIRED IAW ECRA 5330-03388.
- [SDR CALA0400697](https://openairdocs.org/sdr/CALA0400697.md): Skin · cracked · Oct 29, 2004 · N76355 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > MAINTENANCE NOTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STRINGER 22L, BETWEEN STA 727D AND 727E. THE SKIN WAS REPAIRED IAW ECRA 5330-03388.
- [SDR CALA0400615](https://openairdocs.org/sdr/CALA0400615.md): Skin · cracked · Aug 25, 2004 · N76355 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A 2.5 INCH CRACK WAS FOUND IN THE RT FUSELAGE SKIN AT STA 727 UNDER THE EMERGENCY EXIT LIGHT. A SKIN REPAIR WAS INSTALLED IAW ECRA 5330-03090.
- [SDR CALA0400582](https://openairdocs.org/sdr/CALA0400582.md): Skin · damaged · Jul 21, 2004 · N76355 · Boeing 7373T0 · Ailerons
  > INSPECTION FOUND THE LT AILERON DAMAGED ON THE LOWER BONDED SKIN PANEL. THE DAMAGE WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5751-01058.
- [SDR CALA0400575](https://openairdocs.org/sdr/CALA0400575.md): Stiffener · corroded · Jul 15, 2004 · N76355 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND APB VERTICAL STIFFENER CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200.
- [SDR CALA0400574](https://openairdocs.org/sdr/CALA0400574.md): Bulkhead · corroded · Jul 15, 2004 · N76355 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND APB WEB CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200.
- [SDR CALA0400573](https://openairdocs.org/sdr/CALA0400573.md): Skin · cracked · Jul 14, 2004 · N76355 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 2 INCH CRACK IN NR 3 SLAT SKIN LOWER EDGE AT RIVET HOLES ADJACENT TO ACTUATOR. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.
- [SDR CALA0400571](https://openairdocs.org/sdr/CALA0400571.md): Seat Track · corroded · Jul 10, 2004 · N76355 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 910-927. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-00-52.
- [SDR CALA0400568](https://openairdocs.org/sdr/CALA0400568.md): Shear Tie · corroded · Jul 7, 2004 · N76355 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR TIE CORRODED IN E&E COMPARTMENT AT STA 360, LBL 5 BETWEEN S28L AND S29L. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND REPAIRED IAW SRM 53-00-07, FIGURE 207, REPAIR 1.
- [SDR CALA0400563](https://openairdocs.org/sdr/CALA0400563.md): Seat Track · corroded · Jul 3, 2004 · N76355 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 907-927. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52.

Next page: https://openairdocs.org/deregistered/N76355-2011-08-11/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 = 'N76355' AND deregistration_id = 'N76355-2011-08-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N76355-2011-08-11/reports

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