N27733

Service difficulty reports · 71

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 = 'N27733' AND registry_match = 'registration'
  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 CALA2013112700869Frame · crackedFRAME 500C RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA5310-047 16. INSTALLED FRAME REPAIR AT FRAME 500C BETWEEN STRINGER 8 & 9 FOR AC OUTLET EXTRUSION IAW EA5310-04716.Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, FrameSDR CALA2013112700868Frame · crackedFRAME 480L BETWEEN STRINGER 8 & 9 CRACKED AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. INSTALLED REPAIR AT STATION 480L BETWEEN STRINGER 8 & 9 IAW EA5310-04716 REV F FIG 3.Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, FrameSDR CALA2013112700880Frame · crackedFRAME 727A RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA 5310-04716. COMPLETED REPAIR OF FRAME 727A RT CRACK BETWEEN STRINGER 8 AND 9 AT INBD HOLE SUPPORT BRACKET EXTRUSION IAW EA 5310-04716 REV FNov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, FrameSDR CALA2013112700879Frame · crackedFRAME 440L HAS CRACK BETWEEN STRINGER 8 & 9 INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA5310-04716. INSTALLED DOUBLER REPAIR AT FRAME STATION 440L BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV F FIG 3.Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, FrameSDR CALA2013112700878Frame · crackedFRAME 440R SHOWS CRACK INDICATION BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION, IAW EA 5310-04716. REPAIRED CABIN FRAME STATION 440R IAW EA 5310-04716 REV F OP 1.Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, FrameSDR CALA2011102800696Pressure Switch · inoperativeNR 1 FUEL FILTER BYPASS LIGHT ILLUMINATED INFLIGHT. PER FIM TASK 73-05-00-810. REMOVED NR 1 ENG FUEL FILTER. NO CONTAMINATION FOUND. REPLACED FILTER PER AMM 73-11-02-400-801. ALSO REMOVED AND REPLACED NR 1 ENG FUEL FILTER DIFF PRESSURE SWITCH AMM 73-34-01.Oct 28, 2011 · N27733 · Boeing 737724 · Fuel Pressure SensorSDR CALA2011052000376Acm · contaminatedDURING LIFT OFF SMOKE BILLOWING OUT OF CAPTAINS SIDE AIRVENT. D ON O2, SMOKE GOGGLE RAN QRH. RETURNED TO EWR REF LP'S 4393415, 4383411, 8210336 AND 8210335 FOR CORRECTIVE ACTIONS. ALSO PERFORMED HIGH POWER ENG RUN W/ BLEEDS AND PACKS ON (NR 1 AND NR 2) NO SMJan 30, 2011 · N27733 · Boeing 737724 · Cabin Cooling SystemSDR CALA2010111900586Wire Harness · brokenSUPPORT TASK - EMERGENCY LIGHT WIRE BROKEN AT SEAT ROW 30, O/B LEG. REMOVED AND REPLACED EMERGENCY LIGHT WIRE HARNESS AT SEAT ROW 30 LT IAW CMM 25-25-99. OPS CHECK WILL BE PERFORMED ON EA 4420- 01009 REV E OPS 36 STEP 2A. WORK PERFORMED BY SX992.Nov 19, 2010 · N27733 · Boeing 737724 · Lighting SystemSDR CALA2010091700441Handle · out of positionF/A'S IN REAR GALLEY REPORT AT DOOR (AFT ENTRY) THAT THE OUTSIDE HANDLE IS IN VERTICAL POSITION AND NOT STOWED, AND DEPRESSING INSIDE HANDLE CAUSES OUTSIDE HANDLE TO MOVE. REPOSITIONED HANDLE, OPS CHECK OK. OVERWEIGHT LANDING DID NOT HAPPEN PER FLT CREW.Sep 17, 2010 · N27733 · Boeing 737724 · Passenger/Crew DoorsSDR CALA2009032500165Seal · tornCABIN ALTITUDE WARNING HORN SOUNDED WHILE CLIMBING THROUGH 33,000 FT. QRH PROCEDURE STABILIZED CABIN ALT IN MANUAL MODE, PACKS ON HIGH. PACKS IN AUTO WOULD NOT HOLD CABIN ALTITUDE. PERFORMED AN UNSCHEDULED LANDING IN PHX. BITE TEST DCPC FOUND FAULT 030, TRMar 25, 2009 · N27733 · Boeing 737724 · Pneumatic Distribution SystemSDR CALA2009032400163Failsafe · corrodedSTA 927 FAIL SAFE CHORD CORRODED AT STRINGER 25 RT. REMOVED AND REPLACED FAIL SAFE CHORD FROM S-21R TO FACTORY SLICE AT S-24R, REFERENCE EC/RA 5310-04918, STEP 10. DIP WRITTEN TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM 22 MARCH09. PLANNING TO COMar 23, 2009 · N27733 · Boeing 737724 · Fuselage Main, FrameSDR CALA2009031300140Stringer · corrodedSTRINGER 23R STA 847-867 HAS CORROSION, ACCOMPLISHED REPAIRED PER SRM 53-00-03, REF 5684791 FOR WORK ACCOMP AND 44.0008.Mar 12, 2009 · N27733 · Boeing 737724 · Fuselage Main, Longeron/StringerSDR CALA0800467Skin · corrodedCORROSION AROUND FUSELAGE DRAIN PLUG 8" AFT OF NR 1 VHF COMMUNICATION ANTENNA. REPAIRED IAW ECRA 5330-03805 PART 1, INITIATED A DIP TO ACCOMPLISH INSPECTION OF THE REPAIR PER PART 2 PRIOR TO THE ACCOMPLISHMENT OF 50,000 TOTAL AIRFRAME FLIGHT CYCLES AND REPEATMay 14, 2008 · N27733 · Boeing 737724 · Fuselage Main, Plate/SkinSDR CALA0700034Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 947.5-967, RBL 30-45. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-40-02.Jan 27, 2007 · N27733 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA0700045Intercostal · crackedINSPECTION FOUND A 1/2" CRACK IN INTERCOSTAL BETWEEN STA 328 AND 344, LBL 35. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-42-21.Jan 26, 2007 · N27733 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA0700042Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 312-328, LBL 35. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-42-21.Jan 26, 2007 · N27733 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA0700041Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL BETWEEN STA 280 AND 294.5, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-42-21.Jan 26, 2007 · N27733 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA0700040Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 312-328, RBL 30. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-42-21.Jan 26, 2007 · N27733 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA0700039Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 986.5 BETWEEN LBL 26.5 AND LBL 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01876.Jan 26, 2007 · N27733 · Boeing 737724 · Fuselage Main, Floor BeamSDR CALA0700036Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 986.5 BETWEEN RBL 22.5 AND 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01877.Jan 26, 2007 · N27733 · Boeing 737724 · Fuselage Main, Floor BeamSDR CALA0400254Web · crackedINSPECTION FOUND A 2 INCH CRACK AROUND NUT PLATE OF FORWARD O/B WEB OF WHEEL WELL WEB SKI JUMP AT LBL 50.0. THE LEFT WHEEL WELL O/B WEB ON SKI JUMP WAS REMOVED AND REPLACED IAW SRM 51-40-02.Mar 18, 2004 · N27733 · Boeing 737724 · Fuselage Miscellaneous Structure
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