N14106

Service difficulty reports · 158

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 = 'N14106' 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 CALA2013091100652Unknown · odorON CLIMB OUT THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL BURNING ODOR INSIDE THE FORWARD LAVATORY. THE HOT WATER HEATER WAS TURNED OFF. FLIGHT ATTENDANT REPORTED THE VANITY MIRROR BALLAST FELT ABNORMALLY WARM. FLIGHT DIVERTED TO SNN PERFORMED CONDITIONAL INSep 10, 2013 · N14106 · Boeing 757224 · Air Distribution SystemSDR CALA2013071100480Isolation Valve · malfunctionedLEFT ENGINE BLEED OFF CAME ON TAKEOFF. CYCLED ISOLATION VALVE AND SYS OPERATED NORMALLY IAW CREW COMMENT CYCLED ISO VALVE DURING TAXI BACK TO GATE, NR 1 BLEED CHECKED NORMAL IAW CREW REPORT. ACFT OK TO CONTINUE. NOTE: NO MX PERFORMED OR REQUIRED.Jul 6, 2013 · N14106 · Boeing 757224 · Pneumatic Distribution SystemSDR CALA2013042600242Splice Plate · corrodedAFT CARGO SPLICE PLATE BS 1401, STR 28 & 29 LT HAS CORROSION.Apr 25, 2013 · N14106 · Boeing 757224 · Fuselage Main, StructureSDR CALA2011092000613Heater · overheatedPANEL COOLED OFF AND BURN MARK GROWTH STOPPED. RETURNED TO EWR. NO TIME/MAN PWR TO WORK. C/F TO MEL 21-45-2-2R CONTROL NUMBER 567756. OK TO CONTINUE PER MEL. R OW EXIT C/B COLLARED.Sep 20, 2011 · N14106 · Boeing 757224 · Heating SystemSDR CALA2010121000609Oven · malfunctionedOVEN BELOW 103 F/C GALLEY INOP. OVEN BECAME VERY HOT AND STARTED TO OMIT A BURNING ODOR THEN STOPPED WORKING CD TRIPPED FOR OVEN 103. OVEN PLACED ON PLACARD. REMOVED REPLACED OVEN AT 103 F/C GALLEY OPS CHECKED GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT Dec 10, 2010 · N14106 · Boeing 757224 · Buffet/GalleysSDR CALA2010081600390Power Supply · inoperativeEMERGENCY EXIT LIGHTS ON IN REAR OF AIRCRAFT, FRONT LIGHTS OFF WITH ALL SWITCHES IN NORMAL POSITION. REMOVED AND REPLACED M736 & M737 EMERGENCY LIGHTS POWER SUPPLIES AND BATTERY PACKS. REF AMM 33-51-00 & 33-51-07. EMERGENCY LIGHTS CHECK GOOD.Aug 13, 2010 · N14106 · Boeing 757224 · Emergency LightingSDR CALA2010080900383Printed Ckt Board · faultyAURAL FIRE WARNING CAME ON APPROX 10 MINS INTO FLIGHT. COULD NOT EXTINGUISH. PROCEEDED BACK TO EWR FOR AIR RETURN. FOUND AURAL WARNING FIRE GOING OFF CONSTANTLY. REMOVED AND REPLACED M1000 PRINTED CARD. ALL CHECKED GOOD WHEN C/B WAS RESET, AFTER CARD REPLAug 8, 2010 · N14106 · Boeing 757224 · Central WarningSDR CALA2010061000261Failsafe · corrodedAFT CARGO COMPARTMENT-BELT FRAME EXFOLIATED ABOVE S 29L AT STA 1480. REPAIRED BS 1480 LOWER FRAME FAIL SAFE CORD REF ECRA 5311-01492. INTERIM REPAIR ACCOMPLISHED PER ECRA 5311-01492, PART 1. ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 06/07/2010. PJun 10, 2010 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA2010061000265Beltframe · corrodedAFT CARGO COMPARTMENT - BELT FRAME EXFOLIATED ABOVE STR 26 RT STA 1520. REPAIRED BELT FRAME REF SRM 53-00-07 REPAIR 5. ISSUED DIP FOR REP INSPECTION REF 53-00-07 REPAIR 5 FIG 201 TABLE 2 ZONE 1 REQUIREMENTS. REINSPECT BELT FRAME REPAIR STA 1520 ABOVE STRINGJun 9, 2010 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA2010061000264Skin · puncturedSUPPORT TASK: R4 DOOR INTERIOR SKIN HAS SMALL PUNCTURE LOCATED A T UPPER HINGE ARM ASSY. REPAIRED R4 DOOR INNER SKIN AT HINGE CUTOUT REF ECRA 5210-02155 ISSUED DIP FOR PERMANENT REPAIR WITHIN 24 MONTHS. INTERIM REPAIR ACCOMPLISHED PER ECRA 5210-02155, PART Jun 9, 2010 · N14106 · Boeing 757224 · Service DoorsSDR CALA2010061000263Skin · misrepairedEXTERIOR FUSELAGE SKIN STA 630& S28L. EXISTING REPAIR FASTENERS EDGE DISTANCE ED NOT PER SRM. ACCOMPLISHED FUSELAGE SKIN INTERIM REPAIR STA 590-630 S13L TO S 18L REF ECRA 5330-04028. ISSUED DIP INTERIM REPAIR ACCOMPLISHED PER ECRA 5330-04028, PART 1. ACCOJun 9, 2010 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2010061000262Skin · dentedEXTERIOR FUSELAGE SKIN HAS DENT AT STA 754 S17L. REPAIRED EXTERIOR FUSELAGE SKIN STA 750-777 S14L TO S18L. REF ECRA 5330-04027. INTERIM REPAIR ACCOMPLISHED PER ECRA 5330-04027, PART 1. ACCOMPLISH A PERMANENT REPAIR BEFORE 37,500 TOTAL FLIGHT CYCLES. PLANNJun 9, 2010 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2010061000260Sill · damagedSUPPORT TASK: L2 DOOR CUTOUT AT UPPER SILL, OUTER CORD HAS ACCIDENTAL DRILL DAMAGE AT STA 720. REPAIRED UPPER SILL STRAP REF ECRA 5310-05187 ISSUED DIP FOR PERMANENT REPAIR WITHIN 24 MONTHS. INTERIM REPAIR ACCOMPLISHED PER ECRA 5310-05187, PART 1. ACCOMPLIJun 9, 2010 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2010060800249Stringer · corrodedAFT CARGO COMPARTMENT - STRINGER EXFOLIATED AT BS 1472 BL 0. CUT OUT DAMAGED STRINGER SECTION, DRILLED UP NEW SECTION AND REPAIR SPLICE AND INSTALLED ALL REPAIR PARTS. REF SRM 53-60-0 3 AND 53-00-03 REPAIR 1.Jun 4, 2010 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA2010060300247Stringer · corrodedGENERATED DIP FOR N/R 9914225 FOR AFT CARGO COMPARTMENT STRINGER REF SRM 53-00-03 REPAIR 1. EXFOLIATED AT BS 1472 BL 0. 53-DIP CONTROL 05390. INSPECTION THRESHOLD IS 37,500 WITH REPEAT INSPECTIONS OF 3,000 FLIGHT CYCLES. PERFORM INITIAL INSPECTION OF REPAIRJun 3, 2010 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA2010052700226Beltframe · crackedCABIN BELTFRAME CRACKED AT LT SIDE STA 1580 BETWEEN STRINGERS 8LT AND 9LT INSTALLED REPAIR AT STA 1580 LT SIDE BETWEEN STRINGER 8LT AND 9LT. ISSUED DIP 05262 TO PERFORM DETAILED VISUAL INSP AT 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMay 26, 2010 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA2010052700225Beltframe · crackedCABIN BELTFRAME CRACKED AT RT SIDE STA 1580 BETWEEN STRINGERS 8RT AND 9RT. INSTALLED REPAIR AT STA 1580 RT SIDE BETWEEN STRINGER 8RT AND 9RT. ISSUED DIP TO PERFORM DETAILED VISUAL INSP AT 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES May 26, 2010 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA2010052700224Beltframe · crackedCABIN BELTFRAME CRACKED AT STA 760 RT SIDE BETWEEN STRINGERS 8RT AND 9RT. INSTALLED REPAIR AT STA 760 BELTFRAME STRINGER BETWEEN 8RT AND 9RT REF SRM 53-00-07 REPAIR 1.May 25, 2010 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA2009092500568Light · inoperativeEMERGENCY SLIDE LIGHT EXTERIOR FUSELAGE AT MAIN R2 DOOR INOPERATIVE. REPLACED LAMP AT R2 MAIN DOOR EXTERNAL EMERGENCY SLIDE LIGHT, OPERATIONAL CHECKS GOOD.Sep 25, 2009 · N14106 · Boeing 757224 · Emergency LightingSDR CALA0500253Engine · failedNR 2 ENGINE BEGAN TO VIBRATE AT LEVEL OFF AFTER DEPARTING LAX. A RETURN TO LAX WAS INITIATED AND ENG WAS SHUTDOWN ON APPROACH. THE ACFT LANDED WITHOUT INCIDENT. INITIAL EXAMINATION OF THE ENGINE REVEALED METAL IN THE TAILPIPE. THE NR 2 ENGINE WAS R & R IAWAug 4, 2005 · N14106 · Boeing 757224 · Engine (Turbine/Turboprop)SDR CALA0500086Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT FLOORBOARD FASTENER HOLE, BS 720, RBL 26 AND RBL 43.5. REPAIRED IAW ECRA 5320-01769.Mar 21, 2005 · N14106 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA0500085Intercostal · corrodedINSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 334, RBL 2. REPAIRED IAW ECRA 5320-01768.Mar 21, 2005 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA0500087Frame · corrodedINSPECTION FOUND AFT CARGO PIT FRAME CORRODED AT BS 1440, RBL 9, BETWEEN S28R AND S29R. A REPAIR WAS PERFORMED IAW ECRA 5310-04467. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR AFTER 10 MONTHS, BUT BEFORE 3-14-2006.Mar 18, 2005 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA0500079Shear Web · corrodedINSPECTION FOUND SHEAR WEB CORRODED AT BS 1715, BL 0 IN G4 AREA. REPAIRED IAW SRM 53-60-51, FIGURE 203.Mar 14, 2005 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA0500080Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 720, RBL 3 TO LBL 3. REPAIRED IAW SRM 53-00-51, FIGURE 203.Mar 8, 2005 · N14106 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA0400164Sill · corrodedINSPECTION FOUND THE FORWARD CARGO DOOR LOWER SILL UPPER SURFACE CORRODED AT AFT SECTION BEHIND THE SCUFF PLATE SUPPORT BRACKET, STA 580. REPAIRED IAW SRM 51-40-02.Feb 25, 2004 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900272Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO SKIN AT BS 760, STRINGERS 16L-17L. REPAIRED IAW ECRA 5331-01046.Mar 18, 1999 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900271Channel · corrodedINSPECTION FOUND CHANNEL BELOW GALLEY 1A MOUNT BETWEEN STA 345 AND 324, RBL 4 CORRODED. THE CHANNEL WAS REPLACED IAW BOEING DRAWING 141N5161.Mar 17, 1999 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900270Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED AT FS 207.093. REPAIRED IAW SRM 51-70-10, PARAGRAPH 2M, FIGURE 7.Mar 17, 1999 · N14106 · Boeing 757224 · Horizontal Stabilizer, Plate/SkinSDR CALA9900269Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR LOWER EDGE. THE CARGO DOOR LOWER EDGE WAS REPLACED IAW SRM 52-30-03.Mar 17, 1999 · N14106 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900268Stringer · dentedINSPECTION FOUND STRINGERS 3-4L DENTED AT STA 1787. REPAIRED IAW ECRA 5331-01045.Mar 17, 1999 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA9900267Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1640, LBL 52 TO RBL 54. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-01, PAGE 209 TO 213 AND ECRA 5321-01039.Mar 17, 1999 · N14106 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA9900266Panel · damagedINSPECTION FOUND RT WING LEADING EDGE PANEL 611FB DAMAGED AT SCREW HOLE. THE PANEL WAS REPAIRED IAW SRM 51-70-04, PARAGRAPH 4L, AND REFITTED IAW MM 57-41-01.Mar 17, 1999 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900265Panel · delaminatedINSPECTION FOUND RT FIXED L/E PANEL O/B OF PYLON AT WS 320 DELAMINATED. THE PANEL WAS REPAIRED IAW SRM 51-70-08 AND REFITTED IAW BOEING DRAWING 114N2108.Mar 17, 1999 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900264Fairing · delaminatedINSPECTION FOUND LT WING FLAP FAIRING 574CB FORWARD EDGE OUTER SKIN PLIES DELAMINATING. THE FAIRING WAS REMOVED, REPAIRED IAW SRM 51-70-04, AND REFITTED IAW MM 27-51-31.Mar 17, 1999 · N14106 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900263Fairing · delaminatedINSPECTION FOUND FLAP FAIRING 572HB FORWARD EDGE OUTER SKIN PLIES DELAMINATED. THE FLAP FAIRING WAS REMOVED, REPAIRED IAW SRM 51-70-03, AND REFITTED IAW MM 27-51-30.Mar 17, 1999 · N14106 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900262Panel · puncturedINSPECTION FOUND RT HORIZONTAL STABILIZER PANEL NR 345DB PUNCTURED. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-70-05, PARAGRAPH 4C, AND REFITTED.Mar 16, 1999 · N14106 · Boeing 757224 · Horizontal Stabilizer, Plate/SkinSDR CALA9900261Panel · damagedINSPECTION FOUND LT WING LEADING EDGE PANEL NR 521CB DAMAGED. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-70-07, PARAGRAPH 4L, AND REFITTED IAW MM 57-41-01.Mar 16, 1999 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900260Panel · delaminatedINSPECTION FOUND LT WING FIXED LEADING EDGE PANEL OUTBOARD OF PYLON AT WS 320 DELAMINATED. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-70-08, AND REFITTED IAW BOEING DRAWING 114N2108.Mar 16, 1999 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900259Skin · gougedINSPECTION FOUND LT WING O/B UPPER SURFACE INBOARD FLAP PANEL GOUGED BY SPOILER. THE PANEL WAS REMOVED AND REPAIRED IAW ECRA 5753-01061 AND REFITTED IAW MM 57-51-00.Mar 16, 1999 · N14106 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900258Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1520 AND 1560 BETWEEN SRTINGER 29L AND 30L. SKIN REPAIRS WERE INSTALLED IAW ECRA 5331-01044.Mar 16, 1999 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900256Skin · dentedINSPECTION FOUND A DENT IN FUSELAGE SKIN AT BS 620, STRINGER 17L. A REPAIR WAS INSTALLED IAW ECRA 5331-01043.Mar 16, 1999 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900255Panel · gougedINSPECTION FOUND RT WING O/B FLAP UPPER SURFACE INBOARD PANEL GOUGED BY SPOILER. THE PANEL WAS REPAIRED IAW ECRA 5753-01061 AND REFITTED IAW MM 57-51-00.Mar 16, 1999 · N14106 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900254Stringer · crackedINSPECTION FOUND A 4 INCH CRACK IN AFT HOLD FLOOR STRINGER AT STA 1325, RBL 11.5. A REPAIR WAS INSTALLED IAW ECRA 5321-01040.Mar 15, 1999 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA9900253Stringer · crackedINSPECTION FOUND A 6 INCH CRACK IN FLOOR SUPPORT STRINGER AT STA 1400 ABOVE STRINGER 29R. THE CRACKED SECTION OF STRINGER WAS REPLACED IAW SRM 53-60-53 AND ECRA 5321-01041.Mar 15, 1999 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA9900252Chord · crackedINSPECTION FOUND A 1 INCH CRACK IN OUTER CHORDS OF BOTH LEFT AND RIGHT MLG WHEEL WELL STRUCTURE AT STA 1147. THE CHORDS WERE REMOVED AND NEW CHORDS WERE INSTALLED IAW BOEING DRAWING 149N7222.Mar 15, 1999 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900241Beam · damagedINSPECTION FOUND IMPACT DAMAGE TO AFT CARGO HOLD DOOR LOWER EDGE BEAM. THE AFT CARGO HOLD DOOR LOWER EDGE BEAM WAS REMOVED AND A NEW LOWER EDGE BEAM WAS FITTED IAW SRM 52-30-02 AND SRM 52-30-03.Mar 10, 1999 · N14106 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900240Structure · damagedINSPECTION FOUND IMPACT DAMAGE TO AFT CARGO DOOR AFT CORNER AND FORWARD CORNER. THE AFT CARGO DOOR AFT AND FORWARD CORNERS WERE REMOVED AND NEW CORNERS WERE FITTED IAW SRM 52-30-02.Mar 10, 1999 · N14106 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900239Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN BETWEEN NR 7 AND NR 8 SLATS AT OSS 421. REPAIRED SKIN IAW ECRA 5721-01009. A DIP WAS ISSUED TO REINSPECT REPAIR EVERY 1,000 FLIGHT HOURS AND MAKE A PERMANENT REPAIR WITHIN 18 MONTH OR AT NEXT 4C-CHMar 10, 1999 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900238Skin · crackedINSPECTION FOUND A 10 INCH CRACK IN LT WING LEADING EDGE SKIN BETWEEN NR 3 AND NR 4 SLATS AT OSS 421. REPAIRED SKIN IAW ECRA 5721-01009. A DIP WAS ISSUED TO REINSPECT REPAIR EVERY 1,000 FLIGHT HOURS AND MAKE A PERMANENT REPAIR WITHIN 18 MONTHS OR AT NEXT 4C-Mar 10, 1999 · N14106 · Boeing 757224 · Wing, Plate/Skin
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