# Service difficulty reports: N432FE, cancelled May 10, 2010

A list on [N432FE, cancelled May 10, 2010](https://openairdocs.org/deregistered/N432FE-2010-05-10.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 · 95 reports

- [SDR FDEA200805221955](https://openairdocs.org/sdr/FDEA200805221955.md): Engine · failed · May 22, 2008 · N432FE · Airbus A310203 · Engine (Turbine/Turboprop)
  > ON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT INTERMITTENT SQUEAL W/
- [SDR 08FDEA01955](https://openairdocs.org/sdr/08FDEA01955.md): Engine · failed · May 22, 2008 · N432FE · Airbus A310203 · Engine (Turbine/Turboprop)
  > ON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LEFT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT INTERMITTENT SQUEAL W
- [SDR 07FDEA03773](https://openairdocs.org/sdr/07FDEA03773.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT COUPLING, C 65, P 56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03771](https://openairdocs.org/sdr/07FDEA03771.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT COUPLING, C 70, P 37RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03770](https://openairdocs.org/sdr/07FDEA03770.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT COUPLING, C 65, P 56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03769](https://openairdocs.org/sdr/07FDEA03769.md): Plate · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT GROUND VALVE PLATE C 24-25, P52-55 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03767](https://openairdocs.org/sdr/07FDEA03767.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT COUPLING P 55RH, C 65. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03766](https://openairdocs.org/sdr/07FDEA03766.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT COUPLING P 53LT, C 55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03765](https://openairdocs.org/sdr/07FDEA03765.md): Fitting · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03764](https://openairdocs.org/sdr/07FDEA03764.md): Fitting · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03756](https://openairdocs.org/sdr/07FDEA03756.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON COUPLING P 50 RH, C 69. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03754](https://openairdocs.org/sdr/07FDEA03754.md): Stringer · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER P 54 RT, C 68-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03751](https://openairdocs.org/sdr/07FDEA03751.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT COUPLING AT C 65, P 57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03750](https://openairdocs.org/sdr/07FDEA03750.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT COUPLING AT C 65, P 55 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03747](https://openairdocs.org/sdr/07FDEA03747.md): Coupling · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT COUPLING AT C 26/32, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03746](https://openairdocs.org/sdr/07FDEA03746.md): Angle · corroded · Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON REINFORCING ANGLE AT C38-39, P 48 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03672](https://openairdocs.org/sdr/07FDEA03672.md): Panel · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Nacelle/Pylon, Attach Fittings
  > FOUND CRACK ON PYLON NR 2 AT RIB 8 INBOARD AND OUTBOARD SIDE AT PANEL (ABOUT 8MM) DOUBLER REPAIR ON SIDEWALL PANELS PERFORMED IAW SRM 5451-31 FIG 201.
- [SDR 07FDEA03646](https://openairdocs.org/sdr/07FDEA03646.md): Beam · cracked · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Structure
  > FOUND CRACK ON LONGITUDINBAL BEAM C 74-76, P 11 LT/RT, (LT: 8MM, RT 15MM). REPAIR PERFORMED BY INSTALLING REPAIR ANGLES IAW SRM 53-181-18 FIG 204.
- [SDR 07FDEA03684](https://openairdocs.org/sdr/07FDEA03684.md): Skin · damaged · Sep 13, 2007 · N432FE · Airbus A310203 · Trailing Edge Flaps
  > DURING FUNCTION PHASE, THE RT INBOARD FLAP TRAILING EDGE WAS DAMAGED REPAIR PERFORMED IAW SRM 57-53-12 PARA 13 (FIG 209).
- [SDR 07FDEA03707](https://openairdocs.org/sdr/07FDEA03707.md): Flange · damaged · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUR MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
- [SDR 07FDEA03705](https://openairdocs.org/sdr/07FDEA03705.md): Flange · damaged · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > TWO MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
- [SDR 07FDEA03704](https://openairdocs.org/sdr/07FDEA03704.md): Frame · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Frame
  > FOUND CORROSION AT MILLING FRAME C60, P 22RT REPAIR PERFORMED BY BLEND OUT CORROSION IAW RAS/DATLS/0001942/2004.
- [SDR 07FDEA03703](https://openairdocs.org/sdr/07FDEA03703.md): Flange · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON UPPER FLANGE C25. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10
- [SDR 07FDEA03701](https://openairdocs.org/sdr/07FDEA03701.md): Splice · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT SPLICE C20, P50 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03700](https://openairdocs.org/sdr/07FDEA03700.md): Splice · cracked · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT SPLICE C20, P46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03697](https://openairdocs.org/sdr/07FDEA03697.md): Rib · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Rib/Bulkhead
  > FOUND ON LT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 I
- [SDR 07FDEA03696](https://openairdocs.org/sdr/07FDEA03696.md): Rib · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Rib/Bulkhead
  > FOUND ON RT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 IS
- [SDR 07FDEA03690](https://openairdocs.org/sdr/07FDEA03690.md): Skin Panel · worn · Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Plate/Skin
  > ELONGATED HOLES FOUND ON RT WING TO PYLON HYDRAULIC FITTING RIB 8 REPAIR PERFORMED BY REAM UP AND BUSH INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-79595 AND RAS/BAE/0931/2004 ISS A.
- [SDR 07FDEA03688](https://openairdocs.org/sdr/07FDEA03688.md): Skin Panel · worn · Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Plate/Skin
  > FOUND ELONGATED HOLES ON LT WING TO PYLON HYDRAULIC FITTING HOLES RIB 8 REPAIR PERFORMED BY REAM UP AND INSTALL BUSHINGS IAW DRAWING R572-49184, APPROVED BY EA 6-5720-79594 AND RAS/BAE/0931/2004 ISS A.
- [SDR 07FDEA03686](https://openairdocs.org/sdr/07FDEA03686.md): Vane · dented · Sep 13, 2007 · N432FE · Airbus A310203 · Trailing Edge Flaps
  > FOUND DENT ON LT INBOARD FLAP VANE NOSE SKIN, RIB 7-8 REPAIR PERFORMED BY CUTTING THE DAMAGED AREA AND INSTALLING A NEW SKIN WITH INNER STRAPS IAW EA 6-5752-81059 AND RAS/DABRE/7004146/2004 ISS A.
- [SDR 07FDEA03682](https://openairdocs.org/sdr/07FDEA03682.md): Skin · delaminated · Sep 13, 2007 · N432FE · Airbus A310203 · Trailing Edge Flaps
  > FOUND ON LT INBOARD FLAP LOWER SKIN AT TRAILING EDGE, RIB 3-4, DELAMINATION. IN THIS AREA FOUND ON UPPER SKIN AN OLD DOUBLER INSTALLED. REPAIR PERFORMED BY REMOVAL OF THE OLD REPAIR ON UPPER SKIN AND RENEW THE REPAIR ON LOWER AND UPPER SURFACE IAW SRM 57-
- [SDR 07FDEA03681](https://openairdocs.org/sdr/07FDEA03681.md): Skin · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Plate/Skin
  > DURING REMOVAL OF BOLT 642, NOTED IN SB A310-57-2028 FOUND CORROSION INSIDE THE FITTING BORE, LT WING AREA OF RIB 5 REPAIR PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5721-81050 AND RAS/BAE/0928/2004 ISS A.
- [SDR 07FDEA03679](https://openairdocs.org/sdr/07FDEA03679.md): Spar · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Elevator, Spar/Rib
  > CORROSION FOUND ON RT ELEVATOR FRONT SPAR WEB NEAR RIB 2A AROUND ONE BONDING POINT REPAIR PERFORMED BY BLENDOUT UNTIL CORROSION REMOVAL IAW EA 6-5520-79603 AND RAS/CASA/3692/2004 ISS A.
- [SDR 07FDEA03675](https://openairdocs.org/sdr/07FDEA03675.md): Skin · worn · Sep 13, 2007 · N432FE · Airbus A310203 · Nacelle/Pylon, Plate/Skin
  > FOUND ON PYLON NR 1 AT RIB 8 INBOARD AND OUTBOARD SIDE THE HOLE FOR SUPPORT WORN DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.
- [SDR 07FDEA03673](https://openairdocs.org/sdr/07FDEA03673.md): Fitting · worn · Sep 13, 2007 · N432FE · Airbus A310203 · Wing Miscellaneous Structure
  > AT RT SPIGOT FITTING FWD OUTBOARD SIDE FOUND WEAR MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-79605 AND RAS/BAE/0818/2004 ISS A.
- [SDR 07FDEA03671](https://openairdocs.org/sdr/07FDEA03671.md): Attach Fitting · chafed · Sep 13, 2007 · N432FE · Airbus A310203 · Nacelle/Pylon, Attach Fittings
  > FOUND CHAFING MARKS, ENLARGED HOLES AND NOT CORRECT INSTALLED BUSHINGS AT PYLON NR 2 PYLON TO WING ATTACH FITTING LUGS AT RIB 12. REPAIR PERFORMED BY OVERSIZING THE BORES AND INSTALLING NEW REPAIR BUSHS IAW DRAWING R571-40283, APPROVED BY EA 6-5450-81064 AND
- [SDR 07FDEA03667](https://openairdocs.org/sdr/07FDEA03667.md): Fitting · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FOUND CORROSION AT RUN OUT FITTING AT P 44, C16A-17A LT. REPAIR PERFORMED BY REPLACEMENT OF RUNOUT FITTING IAW DRAWING R536-10440.
- [SDR 07FDEA03666](https://openairdocs.org/sdr/07FDEA03666.md): Skin Panel · dented · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > FOUND DENT ON SKIN C 94-95, P3-4 RT OUT OF LIMIT. DOUBLER REPAIR PERFORMED IAW SRM 53-19-12 FIG 201.
- [SDR 07FDEA03661](https://openairdocs.org/sdr/07FDEA03661.md): Stringer · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER P 56 RT, C 64-65 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03660](https://openairdocs.org/sdr/07FDEA03660.md): Floorbeam · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FOUND CORROSION AT CROSSBEAM C 67, C66. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
- [SDR 07FDEA03657](https://openairdocs.org/sdr/07FDEA03657.md): Stringer · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER P50 AT C80, LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03654](https://openairdocs.org/sdr/07FDEA03654.md): Beam · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Structure
  > CORROSION FOUND ON LOWER SILL BEAM OF AFT CARGO DOOR AT C59A. REPAIR PREFORMED BY TRIM OUT THE AFFECTED AREA AND FABRICATE A STRAP IAW EA 6-5310-79580 AND RAS/DATLS/0001970/2004 ISS A.
- [SDR 07FDEA03652](https://openairdocs.org/sdr/07FDEA03652.md): Skin Panel · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON SKIN PANEL C78/80, P 45-50 RT, IN SERVICE PANEL AREA. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND REPLACING THE TOILET SERVICE DOOR WITH COVER A539-809076-200 IAW EA 6-5330-79575 AND RAS/DATLS/0001961/2004 ISS A.
- [SDR 07FDEA03649](https://openairdocs.org/sdr/07FDEA03649.md): Angle · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AFT PRESSURE BULKHEAD CIRCUMFERENTIAL STRAP, INNER RIM ANGLE AND FRAME COUPLING AT C80/82, P25LH TO 36RH. REPAIR PERFORMED BY CUT OUT OF DAMAGED PARTS, REINSTALLING NEW PARTS IAW DRAWING R539-70603, APPROVED BY 6-5318-79562 AND RAS/DAHAM/40182
- [SDR 07FDEA03643](https://openairdocs.org/sdr/07FDEA03643.md): Stringer · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER P 57 LT, C 69-70 OUT OF LIMIT. STRINGER REPAIR PERFORMED SRM 53-10-14 FIG 201.
- [SDR 07FDEA03639](https://openairdocs.org/sdr/07FDEA03639.md): Stringer · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER CONNECTION AT C80, P 38 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03638](https://openairdocs.org/sdr/07FDEA03638.md): Stringer · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT STRINGER P38, C79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201
- [SDR 07FDEA03636](https://openairdocs.org/sdr/07FDEA03636.md): Skin Panel · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INTERNAL SKIN C-37-38, P55LT-55RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 221 AND 203.
- [SDR 07FDEA03635](https://openairdocs.org/sdr/07FDEA03635.md): Stringer · corroded · Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > FOUND CORROSION AT STRINGER P 37 RT, C37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03584](https://openairdocs.org/sdr/07FDEA03584.md): Stringer · corroded · Sep 11, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON CLIP AT C 71, P57-56RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Next page: https://openairdocs.org/deregistered/N432FE-2010-05-10/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 = 'N432FE' AND deregistration_id = 'N432FE-2010-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N432FE-2010-05-10/reports

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