N27610, cancelled May 14, 2012

Service difficulty reports · 43

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 = 'N27610' AND deregistration_id = 'N27610-2012-05-14'
  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 CALA2012031900188Skin · dentedREF L/P 7810838 FOR RECORD OF DAMAGES 6 X 1.6 X 0.090 DEEP ON FUSELAGE BETWEEN STATIONS 767 TO 787 BETWEEN STRINGERS 15R AND 16R. EC/RA 5330-03726 COVERS THREE AREAS OF DAMAGE.Mar 10, 2012 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA2011120700794Wire Harness · defectiveAPU FIRE INDICATION ON CLIMBOUT AT FL240. APU HANDLE WAS PULLED AND BOTTLE DISCHARGED. REPLACED HARNESS M/E 24-2611-3-0003 IAW WDM 26-11-31 RE N/R4479597. ALSO REPLACED M717 (APU TAILPIPE OVERHEAT DETECTOR P/N 10-61096-217) AND M515 (APU TAILPIPE DETECTOR PDec 3, 2011 · N27610 · Boeing 737524 · Fire Protection System WiringSDR CALA2011101400663Unknown · odorTHEN GOT FULL FIRE WARNING LIGHT& BELLS RAN QRH DISCHARGED BOTTLES. FLT ATTENTANT CALLED UP, REPORTED SMELLED SMOKE, CALLED FOR FIREMEN AND WHEN THEY OPENED CARGO DOOR THEY SMELLED SMOKE. PERFORMED CONDITIONAL INSPECTION FOR SMOKE/ODOR IN CABIN/FLIGHT DECK IAOct 14, 2011 · N27610 · Boeing 737524 · Air Distribution SystemSDR CALA2011021500093Warmer · odor1.5 HR INTO FLT, F/A'S REPORT THE BURNT WIRE SMELL IS BACK. DOES NOT APPEAR TO BE COMING FROM AIR VENT BUT IS PRESENT IN ACFT GALLEY. COFFEEMAKERS & OVENS WERE OFF AND NOT USED. TURNED OFF GALLEY POWER. F/A REPORT SMELL LIGHTER NOW, 10-15 MINUTES LATER OPSFeb 15, 2011 · N27610 · Boeing 737524 · Buffet/GalleysSDR CALA2010061400278Connector · defectiveCLIMBING OUT OF AT 18,000FT STARTED TO GET INTERMITTENT APU FIRE WARNING FOLLOWED IMMEDIATE ACTION ITEMS & QRH. DECLARED AN EMERGENCY & RETURNED TO CLE. ON ARRIVAL, APU FIRE WARNING WAS GOING OFF INTERMITTENTLY AGAIN THRU LANDING. TROUBLESHOT APU FIRE DETECJun 12, 2010 · N27610 · Boeing 737524 · Fire Protection System WiringSDR CALA2010051000192Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 344 BETWEEN LBL 10 AND RBL 10 SEE WORK CARD MASTER PANEL CLOSE ZONE 107C SEQ 1007 FOR FLOOR PANELS INSTALLATION. REPAIRED CABIN FLOORBEAM STA 344 UPPER CORD BETWEEN BLL 10 AND RBL 10 PER ECRA 5310-01490.May 9, 2010 · N27610 · Boeing 737524 · Fuselage Main, Floor BeamSDR CALA2010050400186Seat Track · damagedRIGHT O/B SEAT TRACK 6 INCHES FWD OF STA 807 IS DAMAGED. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION OF TRACK REF SRM 53-00-52 REPAIR 4 OPTION 2.May 3, 2010 · N27610 · Boeing 737524 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2010050400184Frame · crackedFRAME STA 360 CRACKED BETWEEN STR 8L&9L AT A/C OUTLET EXTRUSION ATTACHMENT REPAIRED CABIN FRAME STA 360 L/T PER ECRA 5311-01488 AND GENERATED DIP PER PER ECRA 5311-01488 STEP 11 ON N/R LOG PAGE 9716560, SEQ N00714 STEP 12 ON N/R LOG PAGE 9716559, SEQ N00715 ATApr 30, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010043000179Beam · corrodedCORROSION AT L1 DOOR LWR SILL BEAM DOOR CHORD BETWEEN STA 300 AND 360. INSTALLED NEW CHORD AT L1 DOOR LWR SILL BEAM AREA REF SRM 51-40-02.Apr 29, 2010 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA2010042900176Frame · crackedSUPPORT TASK - FRAME WEB OVAL HOLE CRACKED .5 INCH LONG AT STA BS 303.9 AND STRINGER S16L AREA. TRIMMED OUT CRACKED SECTION OF FRAME & SPLICED IN NEW SECTION PER EA5310-04659 OP 2.Apr 29, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042800175Hinge Fitting · crackedL-1 DOOR JAMB, LOWER HINGE FITTING CRACKED ABOVE WL 236.68 AND JUST AFT OF STA 303.9. REMOVED AND REPLACED L-1 DOOR LOWER HINGE FITTING PER SRM 51-40-02.Apr 28, 2010 · N27610 · Boeing 737524 · Passenger/Crew DoorsSDR CALA2010050400183Skin · crackedCRACK FUSELAGE BETWEEN S-8L AND S-9L.Apr 27, 2010 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA2010042700173Frame · crackedFRAME 907 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT(MARKED). FRAME AT STA 907 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.Apr 26, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042700172Frame · crackedFRAME 867 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 867 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.Apr 26, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042700171Frame · crackedSUPPORT TASK PAX CABIN FRAME AT STA 440 BETWEEN STR 8L AND 9L HAS CRACKED INDICATION WHEN PERFORMED HFEC PER EA 5310-04498 OP2. FRAME AT STA 440 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.Apr 26, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042700170Frame · crackedFRAME 400 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 400 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.Apr 26, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042700169Frame · crackedSUPPORT TASK PAX CABIN FRAME STA 440 BETWEEN SRT 8R AND 9R HAS CRACKED INDICATION WHEN PERFORMED HFEC INSPECTION PER EA 5310-04498 OP20. FRAME AT STA 440 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662 CORApr 26, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042700168Frame · crackedFRAME 380 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 380 STR 8R&9R REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.Apr 26, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042600165Frame · crackedSUPPORT TASK PAX CABIN FRAME STA 727B BETWEEN STR 8R AND 9R HAS CRACKED INDICATION WHEN PERFORMED HFEC PER EA 5310-04498 OP 2. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS (ANGLES), TREATED AND PRIMED REF EA 5310-04498.Apr 25, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042600163Sill · corrodedSUPPORT TASK B737-53-4-0010 L-1 DOOR LOWER SILL WEB IS CORRODED BETWEEN STA 312 & 344. REMOVED AND REPLACED L1 DOOR LOWER SILL WEB REF SRM 51-40-02.Apr 24, 2010 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA2010042600162Door Frame · crackedSUPPORT TASK FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT DOOR STOP ATTACHMENT HOLE AT S-22R REFERENCE EA 5310-0444E REV C. REMOVED AND REPLACED CRACKED FRAME PER SRM 51-40-02.Apr 24, 2010 · N27610 · Boeing 737524 · Fuselage Main, StructureSDR CALA2010042600161Frame · crackedSUPPORT TASK PER EA 5310-04498 OP.2, FRAME CRACKED STA 727B BETWEEN S8L AND 9SL. REPAIRED FRAME STA 727B BETWEEN S-8L AND S9-L REF EA 5310-04498.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042600159Frame · crackedFRAME CRACKED BETWEEN S-8R & S9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED FRAME 787 BETWEEN S-8R AND S-9R REF EA 5310-014498.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042600158Frame · crackedFRAME 747 CRACKED BETWEEN S-8R AND S-9R AT OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED FRAME STA 747R BETWEEN S-8R AND S-9R REF EA 5310-0449 8.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042600156Frame · crackedFRAME 907 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET T EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA5310-04498,OP 02.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042600155Frame · crackedFRAME 867 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA 5310-04498, OP. O2.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042300154Frame · crackedFRAME 827 CRACKED BETWEEN S-8L & S9L AT A/C OUTLET EXTRUSION ATTACHMENT. REPAIRED FRAME 827 LT PER EC/RA 5311-01489.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042300153Frame · crackedFRAME 827 CRACKED BETWEEN S-8R &S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED CRACKED FRAME 827 RT PER EC/RA 5311-01489.Apr 23, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2010042200147Frame · crackedFRAME 400 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA5310-04498, OP.02.Apr 21, 2010 · N27610 · Boeing 737524 · Fuselage Main, FrameSDR CALA2009031700143Transmitter · failedON APPROACH WHILE SETTING THE FLAPS TO 30, GOT A SPLIT FLAPS 17 TO 24. ON G/A PLACED FLAPS TO 15 DEGREES AND FLAPS STAYED AT 17 AND 24, ON DOWNWIND FLAPS CAME UP TO BETWEEN 10 AND 15. PUT FLAPS TO 10 WITH NORMAL INDICATIONS. QAR SHOWED A DELAY FROM FLAP XMTMar 16, 2009 · N27610 · Boeing 737524 · Trailing Flap Position Indicating SystemSDR CALA0700309Sill · corrodedINSPECTION FOUND R-1 DOOR SILL LOWER CHORD CORRODED AT STA 277-360, RBL 113. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jun 18, 2007 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0500050Floorbeam · corrodedINSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT FASTENER HOLES, STA 986.5, LBL 54 TO RBL 54. REPAIRED IAW ECRA 5310-04461.Feb 22, 2005 · N27610 · Boeing 737524 · Fuselage Main, Floor BeamSDR CALA0400481Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AFT OF FORWARD BAG BIN DOOR CUTOUT AT STA 452, S22R. A REPAIR WAS INSTALLED IAW ECRA 5330-03351.May 8, 2004 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0400479Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5510-01741.May 7, 2004 · N27610 · Boeing 737524 · Horizontal Stabilizer, Plate/SkinSDR CALA0200567Cargo Track · crackedINSPECTION FOUND A 7 INCH CRACK IN TIE DOWN RAIL AT STA 807, RBL 14. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202.Nov 26, 2002 · N27610 · Boeing 737524 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200566Skin · crackedINSPECTION FOUND A 1/8" CRACK IN SKIN OF CO-PILOT'S WINDSHIELD POST AT UPPER R/H CORNER. A DOUBLER WAS INSTALLED IAW SRM 53-10-01.Nov 26, 2002 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200565Web · crackedINSPECTION FOUND A 2" CRACK IN WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 25, 2002 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200562Angle · crackedINSPECTION FOUND A 1" CRACK IN ANGLE AT STA 500-520, BL O. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.Nov 24, 2002 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200561Angle · crackedINSPECTION FOUND A 1" CRACK IN ANGLE AT STA 344-360, LBL 12. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 24, 2002 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200560Skin · dentedA DENT WAS DISCOVERED IN FUSELAGE SKIN AT STA 360 ABOUT 3" ABOVE CUSP LINE AND 22" AFT OF L-1 DOOR. INSTALLED DOUBLER IAW SRM 53-00-01.Nov 23, 2002 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200357Wire · out of positionTHE WHITE EMERGENCY PATH LIGHT AT SEAT 18C WAS FOUND INOPERATIVE DUE TO A PULLED WIRE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-81.Jun 19, 2002 · N27610 · Boeing 737524 · Light System WiringSDR CALA0000742Window · out of adjTHE R-2 SLIDING COCKPIT WINDOW REQUIRED EXCESS FORCE TO LATCH AND UNLATCH. THE R-2 SLIDING WINDOW WAS ADJUSTED IAW MM 56-12-11, PAGE 501-511.May 25, 2000 · N27610 · Boeing 737500 · Flight Compartment WindowsSDR CALA9701713Battery Pack · dischargedINSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT RIGHT OVERWING AND AISLE RIGHT SIDE, ROW 7 AND 8. THE BATTERY PACK WAS REMOVED AND REPLACED.Dec 9, 1997 · N27610 · Boeing 737524 · Emergency Lighting
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