N323FE, cancelled Jul 23, 2012

Service difficulty reports · 31

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

Query with SQL
duckdb -csv -c "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 = 'N323FE' AND deregistration_id = 'N323FE-2012-07-23'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 04FDEA03390Seal · failedNR 3 PNEU MANIFOLD FAILURE LIGHT ILLUMINATED INTERMITTENTLY SHORTLY AFTER T/O (NR 3 PNEU SUPPLY ON DUE TO WING ANTI-ICE REQUIRED FOR T/O). PHASE IS ACCOMPLISHED. QRH PROCEDURES COMPLETED. LIGHT WENT OUT IMMEDIATELY AS NR 3 PNEU SUPPLY SELECTOR WAS TURNED OFDec 7, 2004 · N323FE · Doug DC1030 · Pneumatic Distribution SystemSDR 04FDEA02023Skin · dentedRIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER DENTED AT STA 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL 2. FABRICATED REPAIR PARTS IAW DC10 SRM 53-20-00 FIG 6 VOL 1 AND DC10 SRM 53-33-01 VOL 2 FIG 2. INSTAJul 7, 2004 · N323FE · Doug DC1030 · Fuselage Main, Plate/SkinSDR 04FDEA02017Wedge · dentedRIGHT HAND OUTBOARD FLAP NR 2 TRAILING EDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN IAW DC10 SRM 51-40-02 VOL 2.Jul 7, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01934Spar · damagedRIGHT HAND WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED Jul 3, 2004 · N323FE · Doug DC1030 · Wing SparSDR 04FDEA01919Skin · crackedNR 3 ENG PYLON CRACK RIGHT SIDE STA YN 320 ABOVE CORE COWL. TRIMMED OUT CRACK IAW DC10 SRM 54-00-01VOL 2, FABBED DOUBLER & FILLER IAW DC10 SRM 54-00-01 VOL 1, INSTALLED REPAIR IAW DC10 SRM 54-00-01 VOL 1.Jul 3, 2004 · N323FE · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR 04FDEA01918Vane · damagedLEFT HAND INBOARD FLAP VANE, LOWER SKIN DAMAGED AT OUTBOARD STOP. REMOVED AND INSTALLED OVERHAULED VANE AT LEFT HAND INBOARD FLAP IAW FEDEX WORKCARD E-8-5750-7-5002 C PT3.Jul 3, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01920Floorbeam · crackedFWD CARGO PIT FLOORBEAM AT BS 652 IS CRACKED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS LOCATED AND DRILLED IAW DC10 SRM 53-00-01 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 2, INSTALLED REPAIR PARTS IAW DC10 SRM 53-00-01 VOL 1.Jul 3, 2004 · N323FE · Doug DC1030 · Fuselage Main, Floor BeamSDR 04FDEA01921Angle · crackedZONE 316 FORWARD UPPER BULKHEAD ANGLE IS CRACKED AT STATION 2164 BULKHEAD TO FUSELAGE SKIN ATTACH ANGLE AT RBL 8. PERFORMED DYE PEN CHECK, FOUND 1 INCH CRACK, REMOVED DAMAGED ANGLE AND INTERCOSTAL CLIPS IAW DC10 SRM 51-35-01 VOL II. FABRICATED AND INSTALLED Jul 3, 2004 · N323FE · Doug DC1030 · Fuselage Miscellaneous StructureSDR 04FDEA01922Rib · crackedRIGHT HAND INBOARD FLAP, INBOARD TRACK UPPER FAIRING, FORWARD RIB CRACKED. REMOVED CRACKED RIB IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW RIB IAW DAC DWG ARC 2340. INSTALLED RIB IAW DC10 SRM 51-35-01 VOL 2 AND DC10 SRM 51-35-02 VOL 2.Jul 3, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01923Skin · crackedRIGHT HAND INBOARD FLAP, INBOARD, AFT HOIST POINT, SKIN CRACKED/DAMAGED. REMOVED TRAILING EDGE WEDGE, FABRICATED REPAIR DOUBLER IAW DC10 SRM 51-21-01 VOLUME 2. REINSTALLED TRAILING EDGE WEDGE IAW DC10 SRM 51-31-01 VOLUME 1.Jul 3, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01924Skin · dentedRIGHT HAND WING INBOARD AILERON - INBOARD EDGE OF LOWER SKIN SURFACE DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW DC10 SRM 57-00-01 VOLUME 1. INSTALLED REPAIR DOUBLER IAW DC10 SRM 51-35-01 VOLUME 2.Jul 3, 2004 · N323FE · Doug DC1030 · AileronsSDR 04FDEA01925Skin · dentedRIGHT HAND WING INBOARD AILERON UPPER SKIN SURFACE HAS NUMEROUSE DENTS. CHECKED LIMITS ON 58 DENTS, 54 DENTS WITHIN LIMITS, 4 DENTS EXCEEDED SRM LIMITS IAW DC10 SRM 51-30-01 VOLUME II. TWO DENTS ON FORWARD UPPER SURFACE AND TWO DENTS ON AFT UPPER SURFACE DAMJul 3, 2004 · N323FE · Doug DC1030 · AileronsSDR 04FDEA01926Track · chafedRIGHT WING LOWER SURFACE, LEADING EDGE DIRECTLY INBOARD OF NR 9 SLAT DRIVE TRACK IS CHAFED. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 57-55-01 FIGURE 1 PARAGRAPH 2 VOL 3 AND 57-00-01 VOL I FIG 1A, PARAGRAPH 5. FABRICATED AND INSTALLED OUTER SLAT SJul 3, 2004 · N323FE · Doug DC1030 · Leading Edge DevicesSDR 04FDEA01927Skin · gougedRIGHT HAND WING LOWER SURFACE, LEADING EDGE ADJACENT TO NR 8 SLAT IS GOUGED. BLENDED GOUGE IAW DC10 SRM 57-00-01 VOL I, FABRICATED AND INSTALLED DOUBLER IAW DC10 SRM 57-10-00 VOL I, 51-21-01 VOL 2, AND 51-33-01 VOL 2.Jul 3, 2004 · N323FE · Doug DC1030 · Leading Edge DevicesSDR 04FDEA01928Angle · crackedLEFT HAND OUTBOARD FLAP, OUTBOARD SUPPORT FITTING, FAIRING ATTACH STRUCTURE LOWER, INBOARD L-ANGLE BRACKET IS CRACKED. REMOVED L-ANGLE BRACKET IAW DC10 SRM 51-35-01 VOL 2, 51-33-01 VOL 2. FABRICATED ANGLE AND INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL 2 AJul 3, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01929Skin · dentedRIGHT HAND OUTBOARD ELEVATOR HAS NUMEROUS DENTS ON UPPER SURFACE. CHECKED DENTS HIGHEST READING 97887.111, DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-80-01. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 55-10-00 VOL I AND 51-21-01 VOL 2. RECORJul 3, 2004 · N323FE · Doug DC1030 · Elevator, Plate/SkinSDR 04FDEA01930Floorbeam · crackedFLOORBEAM CRACKED UNDER CENTER ROLLER TRAY AT ATTACH POINT STATION 840 LBL 2. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 53-00-01 VOL I, 53-00-01 VOL I, AND 51-21-01 VOL 2.Jul 3, 2004 · N323FE · Doug DC1030 · Fuselage Main, Floor BeamSDR 04FDEA01931Floorbeam · crackedFORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 652 IS CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-12-01 VOL 3, 53-00-01 VOL I AND 51-21-01 VOL 2.Jul 3, 2004 · N323FE · Doug DC1030 · Fuselage Main, Floor BeamSDR 04FDEA01932Shear Tie · corrodedCORROSION AND FLAKING PAINT AND PRIMER AT STATION 1821, LONGERON 51L-51R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 58-00-01 VOL I. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC10 SRM 53-30-00 VOL I, 51-21-01 VOL Jul 3, 2004 · N323FE · Doug DC1030 · Fuselage Main, StructureSDR 04FDEA01933Floorbeam · crackedFORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 775 IS CRACKED. REMOVED CENTER ROLLER TRAY FOR ACCESS. FABRICATED REPAIR FILLER ANGLE, REPAIR ANGLE AND CUT OUT DAMAGED AREA IAW DC10 SRM 53-00-01 VOL I. INSTALLED REPAIR PARTS AT STATION 775 FLOORBEAM IAW DC1Jul 3, 2004 · N323FE · Doug DC1030 · Fuselage Main, Floor BeamSDR 04FDEA01935Spar · damagedRT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPJul 3, 2004 · N323FE · Doug DC1030F · Wing SparSDR 04FDEA01917Vane · delaminatedRIGHT HAND INBOARD FLAP VANE, UPPER SKIN HAS MULTIPLE AREA OF DENTS AND DELAMINATION. REMOVED AND REPLACED WITH OVERHAULED VANE RIGHT HAND INBOARD FLAP VANE IAW FEDEX WORKCARD E-8- 5750-7-5002 C PT4.Jul 3, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01896Wedge · dentedRIGHT HAND OUTBOARD FLAP HAS DENT OUT OF LIMITS AT STATION 478 INBOARD END. REMOVE WEDGE IAW DC10 SRM 51-40-2 VOL 2. REMOVE WEDGE SKIN IAW DC10 SRM 51-40-2 VOL 2, FABRICATED NEW SKIN IAW FED-EX EA 8-57-50-77573 AND DC10 DAC DWG ARC 1949. INSTALLED NEW SKIN Jun 30, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01895Wedge · dentedRT OUTBOARD FLAP NR 2 TRAILING EDGE WEDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN ASSEMBLY IAW DC10 SRM 57-21-01 VOL 2 AND DC10 SRM 51-40-01 VOL 2.Jun 30, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01894Bracket · brokenRIGHT HAND OUTBOARD FLAP INBOARD HINGE HAS A BROKEN BRACKET PART NUMBER ARC 2149-25. DISASSEMBLED HINGE PANEL STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. REMOVED BROKEN BRACKET IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW BRACKET IAW DAC DWG ARC 2149. INSTALLED Jun 30, 2004 · N323FE · Doug DC1030 · Trailing Edge FlapsSDR 04FDEA01893Rub Strip · corrodedLEFT WING FUEL PANEL 536DD LANDING RUB STRIP HAS CORROSION AND PITTING LOWER WING. REMOVED CORRODED RUB STRIP IAW DC10 SRM 51-35-01 VOL 2. FOUND LANDING CORRODED, TRIMMED OUT CORRODED AREA AND FABRICATED EXTERNAL DOUBLER, INTERNAL DOUBLER, 2 EACH SHIMS AND FJun 30, 2004 · N323FE · Doug DC1030 · Wing Miscellaneous StructureSDR 04FDEA01892Wire Harness · arcedRT WING INSIDE NR 3 FUEL TANK THRU ACCESS PANEL NR 634 AT FUEL PROBE WIRE HARNESS HAS CUT WIRE WITH EVIDENCE OF ARCING, LOCATED JUST BELOW ACCESS PANEL. REMOVED AND REPLACED WIRE BUNDLE IAW DC10 MM 20-30-01-2.Jun 30, 2004 · N323FE · Doug DC1030 · Wing System WiringSDR 04FDEA01891Skin · dentedRIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER IS DENTED AT FS 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL I PAGE 6116 NR 2. FABRICATED REPAIR COMPONENTS IAW DC10 SRM 53-20-00 FIG 6 VOL 2 AND DC10 SRM 53-33-Jun 30, 2004 · N323FE · Doug DC1030 · Fuselage Main, Plate/SkinSDR 04FDEA01890Frame · corrodedAREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-Jun 30, 2004 · N323FE · Doug DC1030 · Fuselage Main, FrameSDR 04FDEA01889Frame · corrodedAREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33Jun 30, 2004 · N323FE · Doug DC1030 · Fuselage Main, FrameSDR 03FDEA01049Bulb · burned outUPON LOWERING LANDING GEAR, RECEIVED NO GREEN INDICATION ON EITHER F/O'S PANEL OR S/O PANEL. COMPLETED GO AROUND. TESTED LIGHTS, NO TEST ON GREEN LIGHTS. REPLACED BULBS ON F/O'S PANEL. WORKED. FACT 05JUL03 11:30 DTW ? FOUND BULBS BURNT OUT ON F/O'S ANDJul 5, 2003 · N323FE · Doug DC1030 · Landing Gear Position and Warning
Back to N323FE, cancelled Jul 23, 2012