N17105
Service difficulty reports · 98
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 = 'N17105' 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 = 'N17105' 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 CALA2016091400646Lamp · inoperativeLEFT HALF OF EMERGENCY LIGHTS UNARMED LIGHT INOPERATIVE. REPLACED THE LAMP, OPS NORMAL.SDR CALA2016081200528Lamp · inoperativeEMERGENCY LIGHTS INOPERATIVE AT POSITIONS R1 & R2 DOORS. LT OVERWING, AND AFT DOOR. REPLACED THE LAMPS AND PERFORMED AN OPS CHECK, FOUND NORMAL IAW AMM 33-51-00, AND AMM 33-51-06.SDR CALA2016080900508Skin · damagedDURING PREFLIGHT, FOUND A DENT AT BS 1500 BELOW STRINGER 22R, FOUND WITHIN LIMITS IAW SRM 53-00-01.SDR CALA2016080100476Frame · dentedFRAME DENTED AT BS 1400, STRINGERS 25-26L. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101, CUTOUT DAMAGED SECTION OF FRAME. FABRICATED AN ANGLE SECTION REPAIR IAW SRM 53-00-07 REP J FIG 201. TREATED, PRIMES AND TOP COATED DOUBLER REPAIR ON FRAME IAW SRM 53-0SDR CALA2016080100475Frame · damagedFOUND A DENT ON THE FRAME BS 1360 STRINGERS 25-26L OUT OF LIMITS IAW SRM 53-00-07 FIG 101, CUTOUT DAMAGED AREA, FABRICATED A J REPAIR IAW SRM 53-00-07 REP 5 FIG 201. TREATED, PRIMED, TOP COATED DOUBLER AND FRAME AREA IAW AMM 51-21-04, 51-21-14 AND 51-21-15. SDR CALA2016072800459Frame · dentedFRAME DENTED AT BS 600 STRINGER 24-25L. INSTALLED A FRAME REPAIR IAW SRM 53-00-07, FIG 201 REPAIR 5.SDR CALA2016072800458Frame · damagedFRAME DENTED AT BS 680, STRINGERS 23-24R. CUTOUT FRAME DAMAGED SECTION, FABRICATED A REPAIR IAW SRM 53-00-07 REPAIR 5 FIG 201 DETAIL I.SDR CALA2016072500447Frame · crackedVISUAL CRACK INDICATION ON BS 1580 FRAME AT OVERHEAD BIN RAIL ATTACH BRACKET BETWEEN STRINGERS 8 AND 9L. CUTOUT DAMAGED SECTION OF FRAME, TRIMMED OUT, FABRICATED A REPAIR IAW SRM 53-00-07 REP 1 FIG 202 HEAT TREATED IAW 5602, TREATED AND PRIMED REPAIR AND SDR CALA2016072200442Beam · not reportedFABRICATED REPAIR AT CABIN FLOOR LT CREASE BEAM ANGLE BS 760 INBD IAW SRM 53-00-13, 53-30-13 AND AMM 51-21-14-370-801. FABRICATED REPAIR IAW SRM 53-00-13, 53-30-13 AND AMM 51-21-14-370-801 .SDR CALA2016072200441Beam · corrodedLEFT CREASE BEAM INNER ANGLE CORRODED AT BS 876. INSTALLED A REPAIR IAW SRM 53-00-1 3, FIG 201.SDR CALA2016011500050Circuit Breaker · poppedONCE AUTO THROTTLE WAS SELECTED, RT IRU EICAS ON DC WITH RT FMC FAILURE. CB BUS RT SECT 2 POPPED U080913 FOR INPUT ONLY NORMAL AFTER RESET. REPLACED CB P6 PANEL 115VAC BUS R SECT 2 PRECAUTIONARY WDM 24-51-22.SDR CALA2015051500387Oven · dirtyFOR SDR REPORTING, SDR REPORTED FOR SMOKE FROM OVEN. FOOD RESIDUE, OVEN PLACARDED.SDR CALA2015050100354Landing Gear · fireON TAXI OUT ACFT BEHIND REPORTED SMOKE & FLAMES FROM LT MAIN. RUCKS REPORTED NO FLAMES & SMOKE, NO FIRE INDICATION ON EICAS. APPEARS BRAKE LOCKED UP ON LT REAR OTBD, MAIN TEMP WENT TO 3, EICAS ANTI-SKID LIGHT CAME ON AFTER STOP. FOUND NR 5 TIRE BEARING & CASDR CALA2013090300603Light · inoperativeSUPPORT TASK R4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED R4 EXTERIOR EMERGENCY LIGHT & PERFORMED OPERATIONS CHECK FOUND NORMAL AS PER IAW B757 AMM 33-51-06 & 33-51-00.SDR CALA2011102000678Unknown · malfunctionedON APPROACH GOING TO FLAP POS 25 GOT THE T/E FLAP DISAGREE ICAS. RAN CHECK LIST AND LANDED FLAPS 20 T-S IAW FIM 27-51-00-815-809 PERFORMED A BITE OF THE FSEU NO FAULTS NOTED AT THIS TIME. RAN FLAPS DOWN AND UP. NO FAULTS NOTED. OK TO CONTINUE.SDR CALA2011032300162Lens · detachedEMERGENCY EXIT SIGN AT DOOR 2L DETACHED EXIT SIGN RE-ATTACHED.SDR CALA2010110500521Actuator · leakingRT OVERWING SLIDE FAILED OPS CHECK, ACTUATOR LEAKING (WILL NOT HOLD PRESSURE) REMOVED AND REPLACED RT OVERWING ESCAPE SLIDE ACTUATOR REF AMM 25-65-05. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1446488 S/N OFF 00967 IPC REFERENCE NUMBER 25-65-05-01 ACTUATOR, SDR CALA2010110100509Skin · damagedLT FUSELAGE SKIN DENTED AT EXISTING PATCH REPAIR. LOCATION STA 590-600 JUST UNDER STR 16. INSTALLED REPAIR DOUBLERS AND INIATED DIP07709 TO "ACCOMPLISH INSPECTIONS PRIOR TO 35,800 TOTAL AIRCRAFT CYCLES PER ECRA 5330 -04075, PART 2, CONTACT ENGINEERING AFTER SDR CALA2010102500496Beam · corrodedBELTFRAME AT STA 345 HAS CORROSION FROM STA BL-0 TO LBL-24. CORROSION OUT OF LIMITS. REWORKED CORRODED SECTION OF THE FLOORBEAM REF SRM 523-10-51. TREATED AND APPLIED TO UPPER CHORD WHERE REWORKED. FILLED VOIDS WITH BMS5-95. ACCOMPLISHED ALL REWORK PROCEDSDR CALA2009113000692Power Supply · discharged(MULT-33-3-0004) EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M730 INOP IN FWD CABIN AREA. REMOVED AND REPLACED M730 EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-07. OPS CHECKS NORMAL.SDR CALA2009082600514Battery · dischargedEMERGENCY FLASHLIGHT AT L1 DOOR NOT TESTING. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CHECK GOOD.SDR CALA0800702Hose · rupturedLOST LEFT HYDRAULIC QUANTITY INFLIGHT LANDED AT 227,440 POUNDS VERTICAL SPEED - 264. FOUND DOWNLOCK ACTUATOR HYDRAULIC LINE RUPTURED ON RIGHT-HAND SIDE. REMOVED AND REPLACED RIGHT-HAND DOWNLOCK ACTUATOR, PRESSURE AND RETURN LINES REF AMM 20-10-10. LEAK CHECSDR CALA0500160Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 720, RBL 20.5 TO RBL 50.5. REPAIRED IAW SRM 53-00-51.SDR CALA0500169Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED BETWEEN BS 680 AND 700, RBL 56, WL 208.1. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02.SDR CALA0500166Seat Track · corrodedINSPECTION FOUND SEAT TRACK SECTIONS CORRODED BETWEEN STA 720 AND 740, AT RBL 25 AND RBL 45.5. THE SEAT TRACK SECTIONS WERE REPLACED IAW SRM 51-40-02 AND 51-40-05.SDR CALA0500168Intercostal · corrodedINSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 365-377, RBL 60. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02.SDR CALA9900663Light · inoperativeTHE EMERGENCY PATH LIGHTING ON SEATS 11, 32, AND 34 WERE FOUND INOPERATIVE. THE MODULE AT SEAT 11 WAS TIGHTENED. THE CONNECTOR AT ROW 34 WAS RECONNECTED. THE LIGHT FIXTURE AT ROW 32 WAS REMOVED AND REPLACED. OPERATION OF THE EMERGENCY PATH LIGHTING CHECKEDSDR CALA9900405Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 600 BETWEEN STRINGERS 18L AND 19L. THE SKIN WAS REPAIRED IAW ECRA 5331-01051.SDR CALA9900402Channel · crackedINSPECTION FOUND A .25 INCH CRACK IN RT MLG WHEEL WELL FORWARD SEAL RETAINER SUPPORT CHANNEL. THE SEAL RETAINER SUPPORT CHANNEL WAS REPAIRED IAW SRM 51-70-11.SDR CALA9900395Panel · delaminatedINSPECTION FOUND RT WING INBOARD L/E PANEL NR 611HB DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-08 AND 51-41-01.SDR CALA9900394Panel · delaminatedINSPECTION FOUND LT WING PANEL NR 551BB DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-05 AND 57-51-01.SDR CALA9900393Chord · crackedINSPECTION FOUND A 1 INCH CRACK IN LT MLG WHEEL WELL CHORD AT STA 1147. THE CHORD WAS REPLACED IAW BOEING DRAWING 149N7222.SDR CALA9900392Panel · delaminatedINSPECTION FOUND LT WING LEADING EDGE PANEL NR 511DB DELAMINATED AT ATTACHMENT HOLES. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-04 AND MM 51-40-02.SDR CALA9900391Panel · delaminatedINSPECTION FOUND RT FIXED L/E PANEL DELAMINATED OUTBOARD OF PYLON AT WS 370. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-08 AND MM 51-40-02.SDR CALA9900390Panel · delaminatedINSPECTION FOUND LT FIXED L/E PANEL DELAMINATED OUTBOARD OF PYLON AT WS 320. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-08 AND MM 51-40-02.SDR CALA9900383Skin · delaminatedINSPECTION FOUND LT FIXED LEADING EDGE PANEL DELAMINATED AT WS 590 BETWEEN SLATS NR 1 AND 2. THE L/E PANEL WAS REPAIRED IAW SRM 51-70-07.SDR CALA9900382Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED BETWEEN STA 620 AND 640 AT S16L AND S17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 204. A DIP WAS ISSUED TO INSPECT BLIND RIVETS EVERY 2500 FLIGHT CYCLES AND TO REPLACE THE REPAIR NO LATER THAN 1SDR CALA9900381Skin · delaminatedINSPECTION FOUND THE LT FIXED LEADING EDGE PANEL DELAMINATED AT WS 397. THE L/E PANEL WAS REPAIRED IAW SRM 51-70-07.SDR CALA9900380Skin · gougedINSPECTION FOUND THE RT WING OUTBOARD FLAP INBOARD UPPER PANEL GOUGED BY SPOILER FITTING BOLTS. THE FLAP UPPER PANEL WAS REPAIRED IAW SRM 51-70-10, PAGE 10 AND ECRA 5753-01062.SDR CALA9900379Skin · gougedINSPECTION FOUND LT WING OUTBOARD FLAP INBOARD UPPER PANEL GOUGED BY SPOILER FITTING BOLTS. THE FLAP UPPER PANEL WAS REPAIRED IAW SRM 51-70-10, PAGE 10 AND ECRA 5753-01062.SDR CALA9900376Skin · crackedA PERMANENT FLUSH REPAIR TO FUSELAGE SKIN AT STA 595, BETWEEN S17L AND S16L WAS INSTALLED IAW ECRA 5331-01050. THE AREA HAD PREVIOUSLY BEEN REPAIRED FOR A .375 CRACK AND HAD BEEN PLACED ON DIP.SDR CALA9900358Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN PANEL AT STA 780, STRINGER 15L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01.SDR CALA9900344Beam · damagedINSPECTION FOUND IMPACT DAMAGE TO AFT VERTICAL EDGE BEAM, LOWER BEAM, AFT AND FORWARD CORNER PIECES OF FORWARD CARGO DOOR. THE BEAMS AND CORNER PIECES WERE REPLACED IAW BOEING DRAWING 143N6603 AND SRM 52-3-02.SDR CALA9900343Beam · damagedINSPECTION FOUND IMPACT DAMAGE TO AFT CARGO DOOR LOWER EDGE BEAM AND FORWARD CORNER PIECE. THE LOWER EDGE BEAM AND FORWARD CORNER PIECE WERE REPLACED IAW BOEING DRAWING 143N6603 AND SRM 52-30-02.SDR CALA9900339Angle · corrodedINSPECTION FOUND AFT HOLD THRESHOLD ATTACHMENT ANGLE CORRODED AT BS 1376.5 TO 1443.5. THE ATTACHMENT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-60-53.SDR CALA9801359Panel · crackedINSPECTION FOUND A 9 INCH CRACK IN LT WING UPPER SURFACE OF LEADING EDGE COMPOSITE PANEL AT SLAT NR 3, NR 4 STA OSS 421. REPAIR PLIES WERE CUT OUT AND INSTALLED IAW ECRA 5720-01661. A DIP WAS ISSUED TO INSPECT THE REPAIR EVERY SIX DAYS UNTIL PERMANENT REPAIRSDR CALA9801358Panel · crackedINSPECTION FOUND A 3, 8 AND 2.5 INCH CRACK IN RT WING UPPER SURFACE OF LEADING EDGE COMPOSITE PANEL AT SLAT NR 7, NR 8, STA OSS 421. REPAIR PLIES WERE CUT OUT, SANDED, AND INSTALLED IAW ECRA 5720-01661. A DIP WAS ISSUED TO INSPECT THE REPAIR EVERY SIX DAYS USDR CALA9700069Wire · shortedINSPECTION FOUND EMERGENCY TRACK LIGHTS INOPERATIVE FROM ROW 15 TO 25. MAINTENANCE FOUND A SHORTED WIRE UNDER SEAT 17 THAT WAS BLOWING FUSE ON BATTERY CHARGER. THE WIRE WAS SPLICED AND THE FUSE WAS REPLACED. OPERATION OF THE EMERGENCY TRACK LIGHTS WAS RESTO
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