N14107
Service difficulty reports · 121
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 = 'N14107' 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.
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 = 'N14107' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2018122902677Bulkhead Web · damaged(B757-53-3-0599) APU COMPARTMENT STA 1885 BULKHD RBL-8 SKIN HAS CHAFING WEAR FROM ACCESS DOOR 316AR HOLD CLOSE LATCH. RL013 THIS IS TRANSCRIBED INFORMATION ACCOMPLISHED AND RECORDED ON ST-SAA PAPER N/R NO. 0038512, WORK ACCOMPLISHED BY MECH V919728. FOUND OUT SDR CALA2018122872649Door Frame · cracked(B757-52-3-0108) L2 DOOR FRAME CRACKED AT UPPER HINGE FRAME CUT OUT, 16-64() REF STSAA N/R 0038743 REPAIRED DAMAGE AT L2 DOOR FRAME UPPER HINGE CUT OUT IAW B757-20 0 SRM 52-10-02 REPAIR 1 FIG. 201. THIS IS CATEGORY B REPAIR WITH INSPECTION REQUIREMENTS PER TABSDR CALA2018122872648Door Frame · cracked(B757-52-3-0108) R2 DOOR FRAME CRACKED AT UPPER HINGE FRAME CUT OUT. REF ST SAA N/R 0038736. FOUND CRACK OUT OF LIMITS IAW B757 SRM 52-10-02A1 L=.302. REPAIR ED R2 DOOR FWD FRAME AT UPPER HINGE CUT OUT IAW B757-200 SRM 52- 10-02-R1 FIG 201. THIS IS CATAGORY B SDR CALA2018122402642Door Frame · cracked(B757-52-3-0108) R2 DOOR FRAME CRACKED AT UPPER HINGE FRAME CUT OUT. REF ST SAA N/R 0038736. FOUND CRACK OUT OF LIMITS IAW B757 SRM 52-10-02A1 L=.302. REPAIR ED R2 DOOR FWD FRAME AT UPPER HINGE CUT OUT IAW B757-200 SRM 52- 10-02-R1 FIG 201. THIS IS CATAGORY B SDR CALA2018122002613Skin · dentedFUSELAGE SKIN DOUBLER REPAIR HAS DENT AT APPROX.STA 607,2 INCHES BELOW STGR 16L,16-44(). EXISTING DOUBLER DENTED OUT OF LIMITS PER SRM 53-00-01-F101. REMOVED DOUBLER AND REPLACED, CAT B REPAIR IN ZONE A REF SRM 53-00-01 REPAIR 2 FIG 201 AT STA 600-620, STR 15LSDR CALA2018062201501Line · wornMAIN LANDING GEAR DOORS EICAS AFTER GEAR EXTENSION. TOWER ADV ISED IT ARREARED TO BE THE RIGHT. FOUND A LEAKING RIGHT MAIN LANDING GEAR TRUCK POSITION PRESURE LINE. REPLACED LINE. OPS & LEAK CHECKED GOOD IAW MM 20-10-10.SDR CALA2018062101462Wire · brokenSEAT 24C EMERGENCY LIGHT INOP REMOVED AND REPLACED LIGHT ASSY. NO FIX LIGHT PLACED ON MEL. DEFER PER MEL LIGHT PLACED ON MEL FOUND BROKEN WIRE FROM MAIN EARTH TO LIGHT ASSY IN SEAT TRACK TRUNKING, RECRIMPED CABLE PER SWPM 20-10-13 AND ACP TEST OF EMERGENCY LIGSDR CALA2017121204407Sign · unsecureEMERG EXIT ROW SIGN A/C RIGHT FALLING OFF. RESECURED EMERG EXIT ROW SIGN, NO DEFECTS NOTED.SDR CALA2017120804329Oven · smokeAFT LAV SMOKE EICAS. ISOLATED TO OVEN WHEN LAV DOOR WAS OPENED. REPLACED FAULTY OVEN AT POS 413 IN AFT GALLEY. OPERATIONAL CHECK OK.SDR CALA2017102703815Connector · brokenEMERGENCY LIGHTS AT SEAT 4 AB INOPERATIVE. FOUND THE CONNECTOR UNDER THE SEAT IS BROKEN. REPLACED SEAT WIRE HARNESS. LIGHTS CHECKED GOOD.SDR CALA2017102303750Lens · loose20F EMERGENCY SIGN FALLING DOWN REATTACHED LENS COVER, CHECKS GOOD.SDR CALA2017100903558Sign · looseEMERGENCY LIGHT COMING OFF AT ROW 21AC RIGHT, SECURED THE EXIT SIGN.SDR CALA2017073002445Oven · smokeAFT GALLEY OVEN 412 IS SMOKING WHEN IN USE. REPLACED AFT GALLEY OVEN 412. IN REFERENCE WITH AMM 25-34-00. OPS CHECK GOOD.SDR CALA2017072102286Blades · damagedDURING CLIMB OUT 3K FT. THRUST REDUCED.. STRONG YAW & NOISE FROM LEFT ENGINE. PULLED THRUST, INDICATORS SHOWED NORMAL. AFTER FURTHER INTERROGATION EICAS MESSAGE IS RT ENGINE SURGE BITE. FOUND THE NR 2 ENGINE SEVERAL HPC BLADES DAMAGED IN STAGES 3, 4, 5, 6 THATSDR CALA2017070302090Apu · leakingDIRTY SOCK ODOR DURING TAKEOFF FOR 30 SECONDS, ACCOMPLISH FIM TASK 21-00-01, PAGE BLOCK 301. EXAMINED THE COOLING PACKS FOR OIL CONTAMINATION. FIM TASK 21-00-01 PAGE BLOCK301 CARRIED OUT .OIL FOUND POOLING IN APU SERVICE BAY, BAY CLEANED AND LEAK CHECK CARRSDR CALA2017060401665Unknown · odorON TAKEOFF DIRTY SOCK ODOR FOR 30 SECONDS, THEN DISSIPATED DURING TAKEOFF ROLL PERFORMED FIM TASK 21-00-01 PAGEBLOCK 301. AIR CONDITIONING SYS TEM INSPECTION FOUND OK. NO ODOR NOTICED. OK FOR SERVICE.SDR CALA2017022400443Wedge · crackedDURING CRUISE PASSENGER REPORTED SEEING A GAP BETWEEN LEFT INBOARD SLAT AND WING. EMERGENCY DECLARED. INSPECTED LEFT INBOARD SLAT AND FOUND NR 5 SLAT TRAILING EDGE WEDGE BULGING WITH APPROX 4 INCH CRACK AT CENTER OF WEDGE. REMOVED AND REPLACED LEFT WING MOST ISDR CALA2017010900052Light · inoperativeBOTH BULBS BURNED OUT ON EMERGENCY LIGHTS DISARMED LIGHT. RELAMPED OPS CK OK.SDR CALA2016111800926Lens · missingFOUND L2 DOOR EMERGENCY LIGHT LENS COVER OFF. REPLACED THE EMERGENCY SIGN LENS. OPS CHECKED OK.SDR CALA2016111400912Light · inoperativeRT AFT SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED RIGHT AFT EXTERIOR EMERGENCY LIGHT, OPS CHECKS GOOD.SDR CALA2016011500054Strap · corrodedCORROSION ALONG APU INLET DOOR AFT SUPPORT AT STATION 1825, BETWEEN STRINGER 3R - 6R. CUT OUT DAMAGED INNER STRAP, FABRICATED REPAIR PIECES, TREATED, PRIMED & INSTALLED IAW SRM 53-80-15 REPAIR 1 & ECRA 5380 -01117.SDR CALA2016011200049Frame · wornRIGHT BELT FRAME AT STATION 1640, STRINGER 6 RT, SHOWS WEAR MARK. REPAIRED FRAME IAW ECRA 5310-06728. PLACED ON DIP, CONT 95720 IAW STEP 17 OF ECRA 5310-06728. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 37,000 TOTAL FLIGHT CYCLES. PLSDR CALA2016010800040Floorbeam · corrodedFORWARD WET AREA FLOORBEAM AT STATION 377.5, LBL 0 TO 12 INCHES HAS CORROSION. REPAIRED FWD WET AREA FLOORBEAM IAW ECRA 5300-02286.SDR CALA2016010800030Frame · crackedCABIN STATION 760, BETWEEN STRINGER 8L & 9L, BELT FRAME CRACKED AT INBD RIVET. INSTALLED FUSELAGE FRAME REPAIR. PLACED IN DIP TO DO VISUAL INSPECTION EVERY 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, OR 50,000 AIRFRAME CYCLES, WHICHEVER CAME FIRST IAW SRMSDR CALA2016010400021Frame · crackedBELL FRAME LOCATED AT BS 1120 LT HAS CRACK AROUND FASTENER HOLE LOCATED BETWEEN STRINGER 6L & 9L. CUT OUT DAMAGED SECTION FRAME & INSTALLED REPAIR. INITIATED A ZONE 3 DIP OF A RIVETED FRAME REPAIR TO RE-INSPECT AT 12000 FLIGHT CYCLES FROM REPAIR INSTALLATIONSDR CALA2015123001050Beltframe · crackedCABIN STATION 760, BETWEEN STRINGER 8R & 9R, BELT FRAME CRACKED AT INBD RIVET. INSTALLED FUSELAGE FRAME REPAIR. PLACED IN DIP TO DO A VISUAL INSPECTION EVERY 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, OR 50,0000 AIRFRAME CYCLES, WHICHEVER COMES FIRST IAWSDR CALA2015122801032Frame · crackedBELL FRAME LOCATED AT BS 1120 RT HAS CRACK AROUND FASTENER HOLE, LOCATED BETWEEN STRINGER R8 & R9. REPAIRED IAW SRM 53-00-07 REPAIR 1. INITIATE DIP 53, DIP CONTROL 95343 FOR THRESHOLD DVI AT 12000 CYCLES & 50000 TOTAL CYCLES WHICHEVER COMES FIRST. REPETITIVSDR CALA2015122401026Frame · crackedCABIN STATION 800, STRINGER 8R & 9R, BELT FRAME CRACKED AT INBD RIVET. CUT OUT DAMAGED SECTION OF FRAME & INSTALLED REPAIR. INITIATED A ZONE 3 DIP OF A RIVETED FRAME REPAIR TO RE-INSPECT AT 12 ,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME CYCLES, WSDR CALA2015122101008Attach Bracket · crackedLEFT PSU RAIL ATTACH BRACKET AT BELT FRAME SHOWS CRACK AT FASTENER STATION 1580. CUT OUT DAMAGED SECTION OF FRAME & INSTALLED REPAIR.SDR CALA2015071500567Unknown · malfunctionedFOR SDR REPORTING, LOW SPEED ABORT UNDER 20 KTS ON TAKEOFF, AUTO THROTTLE ISSUE. DEFERRED LOG PAGE 7495441 INBD TAKEOFF. WHEN AUTO THROTTLES SELECTED, LT THROTTLE DIDN’T RESPOND. COLLARED CB F16 TMC SERVO.SDR CALA2015061000498Skin · dentedSKIN DENTED FROM INSIDE OUT BS 375 BELOW STRINGER 22R DIMPLE PROTRUDES OTBD. CUT OUT DAMAGED AREA. FABRICATED & INSTALLED REPAIR IAW SRM 53-00-01 REPAIR 7 FIG 201.SDR CALA2015050400367Coffeemaker · sparksREAR RT COFFEE POT HAD SHOWN SPARKS, CB`S IN GALLEY PULLED. FORM 46.6020 COMPLETED BY FLT CREW & ATTACHED. COMPLIED WITH AMM 05-51-58 WITH COFFEEMAKER AT 416 AT FAULT. REPLACED BOTH COFFEEMAKERS 416 & 415 AS PRECAUTION. OPERATIONS NORMAL WITH NO OTHER DISCSDR CALA2014030300248Transmission · trippedTE FLAP ASYMMETRY WARNING CAME ON WHILE CONFIGURING FOR APPROACH. USED ALTERNATE FLAP SELECTOR TO BRING FLAPS TO 20'' INDICATION. DEBRIEFED CAPTAIN & WORDING ABOVE SHOULD READ TE FLAP DISAGREE NOT ASYMMETRY. FSEU 1 SHOWED FAULT 305. PERFORMED FIM TASK 27- SDR CALA2013081900573Relay · failedAT FL340 AUTO PILOT KICKED OFF & A LOUD BANG WAS HEARD MID ACFT. GALLEY POWER WAS LOST, IFE SYSTEM KICKED OFF & AUTO PILOT, AND AUTO THROTTLES KICKED OFF. STRONG ODOR OF SMOKE FROM F/C SECTION TO MID WING PRESENT RT RECIRCULATION FAN EICAS MESSAGE. DIVERTED. SDR CALA2013022500128Skin · dentedAFT CARGO DOOR HAS DENTS ON 2 LIGHTNING HOLE CUTOUTS. CUT OUT DENT DAMAGE AT TWO LIGHTNING HOLES ON AFT CARGO DOOR INNER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLERS REF EC/RA 52 32-01150, REV A.SDR CALA2011032900219Reflector · defectiveL-4 DOOR EMERGENCY EXIT LIGHT INOP (EXTERIOR LIGHT). RELAMP, NO HELP. CHECKED FUSES ON M737, ALL FUSES CHECK GOOD. REPLACED F1 FUSE, NO HELP. FOUND L56 INTERMITTENT. REQ'S LIGHT ASSY, NIS LAX. PLACARD L-4 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED SOCKET SDR CALA2010122200633Girt Bar · malfunctionedDOOR 1R ON DESCENT WENT FROM ARMED TO DISARMED PERFORMED GIRT BAR MECHANISM SYSTEM TEST AS PER 52-11-25-735-024. ALSO PERFORMED GIRT BAR MECHANISM ADJUST TEST AS PER 52-11-25- 825-001, ALL OPS CHECKS NORMAL, AS PRECAUTION PRESSURIZED A/C, NO FURTHER DEFECT NOSDR CALA2010072700348Fan · malfunctionedELECTRICAL WIRE SMELL CAME FROM F/O VENT AREA UNDER EFB FOR 2 MIN AND WENT AWAY DURING DESCENT, SMELL CAME BACK FOR APPOX 2 MIN & WENT AWAY PERFORMED INSP OF FWD E&E COMPARTMENT . REMOVED AND REPLACED RT RECIRC FAN AS A PRECAUTION, RAN ENGINE TO SIMULATE DISCSDR CALA2010070800330Support Fitting · wornLEFT WING NR 3 FLAP TRACK AFT SUPPORT FITTING FOUND ELONGATED HOLES AT FLAP LOWER PANEL AND LOWER CHORD. REPAIRED AS PER EC/RA 5750-04318 AND FORM 44.0008 ITEMS 1 THRU 9. DIP ISSUED TO "ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 6/29/10.SDR CALA2010070700327Seat Track · corrodedM/D STA 1340-1360 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 1 FIG 201 AT STA 1320 TO STA 1410 LBL 45 AND FORM 44.0008SDR CALA2010070700326Seat Track · corrodedCABIN: STA 1140 - STA 1160 RBL 45 SEAT TRACK LIP FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER AMM 20-11-00 AT CABIN STA 1070 TO STSDR CALA2010070700325Seat Track · corrodedM/D STA 1440-1460 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 1 FIG 201 AT STA 1410-1540 LBL 45 AND FORM 44.0008 ATT ITEM 1-15 ACSDR CALA2010070700324Seat Track · corrodedCABIN STA 1180-1200 RBL 45 SEAT TRACK LIP FOUND CORRODED. SEAT TRACK SCRATCH SMOOTHED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE FIG 101 LIMIT & SEAT TRACK REPLACED AS PER SRM 51-10-02 & NEW SEAT TRACK INSTALLED AS PER AMM 20-11-00 AND SRM 51-40-02 AT STA 1180 TO SSDR CALA2010070700323Seat Track · corrodedCABIN STA 1080-1100 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CROWN CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALLED AS PER AMM 20-11-00 AND FORSDR CALA2010070700322Seat Track · corrodedCABIN STA 1160-1180 LBL 24 SEAT TRACK CROWN AND LIP FOUND CORROSION. CABIN SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER AMM 20-11-00 AT STA 1070 TOSDR CALA2010070700321Seat Track · corrodedM/D STA 1540-1560 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGED 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AT STA 1540 - STA 1600 LBL 45SDR CALA2010070700320Floor Support · corrodedCABIN RT STA 685 RBL 18 FLOOR SUPPORT UPPER SURFACE FOUND CORROSION. CABIN RT STA 685 RBL 18 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT & CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 & NEW SUPPORSDR CALA2010070700319Floor Support · corrodedCABIN STA 355 BL 0 FLOOR SUPPORT UPPER SURFACE CORROSION. CABIN STA 355 BL 0 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW SUPPORT INSTALLED SDR CALA2010070700318Floor Support · corrodedCABIN STA 329 BL 0 FLOOR SUPPORT UPPER SURFACE CORROSION. CABIN STA 325 BL 0 FLOOR SUPPORT SUPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SUPPORT REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-0SDR CALA2010070700317Floor Support · corrodedCABIN RT STA 700-715 RBL 18 FLOOR SUPPORT UPPER SURFACE FOUND CORROSION. CABIN STA 700 TO STA 715 RBL 18 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-10-0
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