N16709
Service difficulty reports · 104
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 = 'N16709' 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 = 'N16709' 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 CALA2026092519803Oven · smokeGALLEY OVEN 423 BEGAN SMOKING AFTER USE. FA TURNED OFF AND REMAINED UNUSED. CIRCUIT BREAKER COLLARED & OVEN DEACTIVATED. STICKER APPLIED. CLEANED AND RESET OVEN 423, WHEN OPERATING OVEN AN ODOR WAS NOTICED. WHEN OVEN OFF, ODOR GONE. PERFORMED SMOKE/ODOR ISDR CALA2026081718692Skin · crackedCRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN AT HSS 157.10 , 9" FROM REAR SPAR, INBD ROW. CRACK LENGTH 1 INCH. ACCOMPLISHED REPAIR OF THE RT HORIZONTAL STAB LOWER SKIN HSS 157.10 & DIP INSPECTIONS WILL BE REQUIRED IAW SRM 55-10-01-2R-11, REPAIR 11, PAGE 7, TSDR CALA2026081318549Spar · corrodedFOUND CORROSION AT LEFT WING INBD FRONT SPAR BOOST PUMP UPPER SIDE. REMOVED CORROSION AT LT WING INBD FRONT SPAR BOOST PUMP UPPER SIDE , FOUND AREA TO BE WITH LIMITS IAW SRM 57-20-10-1A-3.SDR CALA2026021113703Warning Message · false activationSPEED BRAKES DO NOT ARM LIGHT ILLUMINATED IN FLIGHT WITH FLAPS EXTENDED. SPEEDBRAKE LOAD ALLEVIATION SYSTEM HAS BEEN DEFERRED IN COMPLIANCE WITH MEL CARD 27045. PERFORMED INITIAL EVALUATION IAW FIM 27-62 TASK 802, FOUND ERROR TO BE A NUISANCE MESSAGE. THE SDR CALA2026010212603Engine · faultedRTO AT 63 KNOTS. NR 2 ENG STOPPED SPOOLING AT 75 PERCENT, LOG PAGE UPDATED CREW BRIEFED THAT THE 75 PERCENT STATED IN HIS WRITE-UP IS 75 % N1 PERFORMED FIM TASK # 73-05 TASK 814 ENGINE IS SLOW TO ACCELERATE. ALL PARAMETERS NORMAL WITH NO ERRATIC SIGNALS NOTEDSDR CALA2025120811923Module · faultedLANDING GEAR FAILED TO RETRACT ON T/O. MANUAL GEAR EXT DOOR SWITCH DID NOT FIX ISSUE DEBREIFED FLIGHT CREW AND THEY REPORTED THAT ALL LANDING GEAR INDICATORS GREEN/RED WERE ILLUMINATED AFTER FIRST GEAR RETRACTION ATTEMPT. FOLLOWING EMERGENCY PROCEDURE THE GESDR CALA2025101410042Girt Bar · unraveledR1 GIRT BAR HAS ACCESS SLIDE MATERIAL SHOWING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMSDR CALA2025090508513Oxygen Mask · no testCREW OXYGEN MASK REGULATOR TEST. CAPTAIN MASK REGULATOR UNIT HEAD HARNESS LEAKS WHEN TESTED. REMOVED AND REPLACED CAPTAIN MASK REGULATOR IAW AMM 35-12-85. OPS AND LEAK CHECKED OK.SDR CALA2025090508508Battery · inoperativeEMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK - M1670 BATTERY FAILED FUNCTION CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805,. OPS CHECKED GOOD.SDR CALA2025051404666Slide · no discrepancy1R DOOR SLIDE RAFT MATERIEAL IS OUT TOO FAR UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. M VERIFIED DOOR 1R Z FOLD FABRIC WITHIN LIMITS APPROXIMATELY 11 INCHES REF AMM TASK 25-66-01-400-804 OK FOR SERVICE VERIFSDR CALA2025012301992Slide · dislodgedFWD ENTRY DOOR SLIDE IS PARTIALLY STICKING OUT OF CASE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003127480 AND PRTR RE-TUCKED LOOSE SLIDESDR CALA2024123001712Slide · damagedGIRT MATERIAL AT 1L HAS COME OUT OF SLIDE PACK COVER REMOVED AND REPLACED DOOR 1 LEFT SLIDE IAW REF 25-66-01-400-803 .PARTS USED: 29-2566-9-0006,QTY :1 ADD EMP:U260507,U416899 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1334994 SN OFF 9434 SLIDE, FWD/AFT OFSDR CALA2024100100735Proximity Sensor · faultyRIGHT MAIN LANDING GEAR GREEN LIGHT REMAINED ILLUMINATED AFTER DEPARTURE. PROVIDED BY FLIGHT CREW PERFORMED BITE ON PSEU REF AMM 32-09 TASK 801 FOUND EXISTING FAULTS 2, MESSAGE 32-61005, LATCHED AND 32-61004 NOT LATCHED, RIGHT LAND GEAR DOWN LOCK FAULT. UPLOADSDR CALA2023112703474Indicator · inoperativeAT 10000 CABIN ALT WAS -1000FT. CABIN RATE OF CLIMB APPEARED NORMAL AT 28000 DIFFPRES WAS8 VERIFIED QUICK DISCONNECT PROPERLY INSTALLED. ADDING PIC T/S PER FIM 21-33 TASK 803. REMOVED AND REPLACED CABIN ALT AND DIFFERENTIAL PRESSURE INDICATOR, REF AMM 21-33-02SDR CALA2023101303057Charger · inoperativeSUPPORT TASK EMERGENCY LIGHTS CONNECTED TO BATTERY CHARGER M1668 STAY ON WITH FLIGHT DECK SWITCH IN OFF REF HAECO GSO NR 9282992. REMOVED AND REPLACED BATTERY CHARGER M1668 IAW B737 AMM 33-51-06-960-806 REF HAECO GSOSDR CALA2023101303056Charger · inoperativeSUPPORT TASK EMERGENCY LIGHTS CONNECTED TO BATTERY CHARGER M1675 STAY ON WITH FLIGHT DECK SWITCH IN OFF REF HAECO GSO NR 9282993 REMOVED AND REPLACED BATTERY CHARGER M1675 IAW B737 AMM 33-51-06-960-806 REF HAECO GSO.SDR CALA2023101303037Battery Pack · inoperativeSUPPORT TASK EMERGENCY BATTERY PACK M1669 NEEDS REPLACED REF HAE CO GSO NR 9282056 REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M1669 RH OVERWING EXIT REF B737-700 AMM 33-51-06-960-805. EMERGENCY LIGHT BATTERY PACK CHECKS GOOD.SDR CALA2023101103024Window Frame · crackedSUPPORT TASK CRACK FOUND IN LH NO. 1 WINDOW FRAME AT STA 1217 WL258 COMING OFF OF THE TOP LEFT INTERNAL FASTENER THAT ATTACHES STEEL CHORD DOUBLER. CRACK MARKED IN RED REF HAECO GSO NR 9282713 CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). RESDR CALA2023092902911Panel · corroded(B737-53-3-0785) AFT CARGO COMPARTMENT WAST TANK WHERE RINS FITTING HEATER TERMOSTAT ATTACHE TO IT THE PANAL IS CORRODED.SDR CALA2023092902903Panel · crackedSUPPORT TASK- R/H HORIZONTAL STABILIZER, UPPER INBOARD PANEL LAND CRACKED AT NUTPLATE LOCATION. TRANSCRIBED FROM HAEC OGSO NRC# 9282697. ACCOMPLISHED UAL ECRA 5516-01043.SDR CALA2023092702884Threshold · corrodedSUPPORT TASK: MAIN CABIN R-2 DOOR THRESHOLD WEB RBL-39 HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC# 9282553 BOEING DWG# 147A8510 REV E. REMOVED .071" CORRODED MATERIAL FROM ORIGINAL .071" THICKNESS. R EMAINING 0 MATERIAL THICKNESS FOUND TO BE OUT OF LIMITSDR CALA2023092702883Deck Plate · corrodedMAIN CABIN STA 992.8, RIGHT HAND DECK WEB PLATE HAS AREAS OF CORROSION. REMOVED .010" CORRODED MATERIAL FROM ORIGINAL .020" THICKNESS. R EMAINING .010" MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-01-1 AND DWG 147A5712 REV-. REMOVE D AND REPSDR CALA2023092702882Door Sill · corrodedSUPPORT TASK: MAIN CABIN R-2 DOOR SILL APPROX STA 986 CHORD HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC# 9282250 REMOVED 50% CORRODED MATERIAL FROM ORIGINAL THICKNESS. FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-70-15 AND BOEING DWG# 147A8501 REV C. REMOVED ASDR CALA2023092702881Skin · dentedAFT CARGO DOOR SKIN DENTED. REMOVED AND REPLACED OUTER SKIN ASSY ON AFT PIT DOOR IAW SRM 52-30-01-2R-3.SDR CALA2023091402783Floorbeam · corrodedSUPPORT TASK: MAIN CABIN STA 986.5 FLOOR BEAM UPPER SURFACE HAS CORROSION AT RBL-36, TRANSCRIBED FROM HAECO GSO N/R 9282552 REMOVED CORROSION FROM STA 986.5 FLOORBEAM AT RBL36 AND RBL5. ORIGINAL MATERIAL THICKNESS .150, REMOVED .015, REMAINING .135 OUT OF LIMISDR CALA2023091402782Frame · corrodedSUPPORT TASK: MAIN CABIN STA 727 STR 1L TO 2L HAS AREA OF CORROSION, TRANSCRIBED FROM HAECO GSO N/R 9282437 REMOVED CORROSION IAW B737-700 SRM 51-10-02 ORIGINAL THICKNESS . 131 REMOVED .031 REMAINING .100. REPAIRED STA 727 FRAME INNER CHORD 51L-52L IAW UNITESDR CALA2023080202407Wire · severedEMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - FWD CLOSET AFT AISLE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY REF MM 33-51-14. NO HELP. SWPM20-30-11 AND REASSEMBLED TERMINAL BLOCK REF SWPM 20-30-00. REMOVED AND REPLACED PWR SUPPLY REF MM 33-SDR CALA2023041201099Panel · missingPANEL MISSING JUST AFT OF R MLG SEE PICS ATTACHED. INSTALLED PANEL P/N 149A7654-8. CHECKS SECURE.OK TO CONT PARTS USED: 29-5351-3-0028,QTY :1SDR CALA2023021000384Fastener · missingPDA 3 RT UPPER WING PANEL MISSING 11 EACH FASTENERS. SEE PHOTO. ADDED PHOTO. INSPECTED NUT PLATES AND REPLACED MISSING SCREWS ON RT WING UPPER PANEL 651BT.SDR CALA2022090502270None · noneAIRCRAFT LAV SERVICE DOOR FOUND MISSING ON INBOUND FLIGHT. SEE PICTURE. GVI WASTE TANK SERVICE PORT AND LH TAIL STRUCTURE. NO DAMEGE FOUND. REPLACED WASTE SERVICE PANEL. OPS CK GOOD.SDR CALA2022081602105Stringer · damagedLONGITUDINAL ANGLE IN HORIZONTAL STABILIZER CENTER SECTION AREA, JUST ABOVE WHERE UPPER RH SLIDING SEAL AFT TRACK TURNS INWARD, IS WORN FROM CONTACT WITH SLIDING SEAL THAT WAS NOT BEING CAPTURED BY SEAL TRACK. SEE PICS. REMOVED UPPER R/H STAB SLIDING PLATE TSDR CALA2022061301491Light · shortedR1 DOOR EMERGENCY LIGHTS NOT WORKING. TROUBLESHOT SYSTEM IAW AMM 33-51-14 AND FOUND SHORTED EMERGENCY LIGHT JUST FORWARD OF SEAT 1A/B VERIFIED ALL RII REQUIREMENTS METSDR CALA2022021600404Strap · looseBOTH NAV1 AND NAV2 SHOW FAIL. NAV1 THRU 10K FT NAV2 15 MIN LATER TS PER FIM 22-15-00 TASK 813. MULTIPLE FAULTS FOUND DURING BITE AFTER CONFERRING WITH TOMC IN REGARDS TO THE NAV TUNING PANEL LIBRARY TEST. FAILURE 1 AND 2, ACMP FIM 34-31 TASK 801 WITH PARTICULASDR CALA2021122702453Seal · missingPDA 3 #6 T/EFGE FLAP FAIRING OUTBD SIDE CENTER SEAL COMPLETELY MISSING -- SEE PHOTO PHOTO ADDED REPLACED MISSING SEAL. REF SRM 57-53-70-2R-2. REPAIR 2 PAR 4 ALTERNATIVE 1 REPAIR.SDR CALA2021072601194Sensor · malfunctioned*EMERGENCY DECLARED* LEADING EDGE SLAT 7 ILLUMINATED. LE FLAP TRANSIT LIGHT ON FWD I LLUMINATED. PER CREW, SELECTED FLAPS 5, LEADING EDGE TRANSIT AND OVERHEAD SLAT 7 STAYED ILLUMINATED FOR APPROX 5 MIN THEN EXTINGUISHED. SELECTED FLAPS 15, SAME... DECLARED EMSDR CALA2020100901167Computer · malfunctionedYAW DAMPER OFF AFTER TAKEOFF. WHEN RE-SELECTED RUDDER ENGAGED ABRUPTLY. FOUND POSITION 1 SMYD FAILED SELF TEST. REMOVED AND REPLACED POSITION 1 SYMD, PER AMM 27-32-42. ALL TESTS PASSED. S/N OFF 0869 COMPUTER, STALL OFF 29-2732-9-0003 0869 ON 29-2732-9-000SDR CALA2020091801123Skin · crackedRT HORIZONTAL STAB HAS CRACK INDICATION AT STAB STA 147.90 APPROX. 25" FROM AFT EDGE, MARKED. SEE FLEET CYCLE N/R 9752929 FOR WORK PERFORMED, PER SRM 55-10-01 REPAIR 11. INSP THRESHOLD 56000 TOTAL FLT CYLCLES, DVI 9000 FLT CYCLES; EXTERNAL LFEDC AT 9000 FLT SDR CALA2020091801117Skin · crackedRT HORIZONTAL STAB HAS CRACK INDICATION AT STAB STA 138.70 APPROX 10 1/4" FROM AFT EDGE. REPAIRED RT HORIZONTAL STAB LOWER SKIN AT STA 138.70 AND 10 1/4" FWD OF AFT EDGE, REF SRM 55-10-01 REPAIR 11 FIGURE 204 DETAIL "F". WORK PERFORMED ON FLEETCYCLE N/R 9752SDR CALA2020071201046Light · malfunctionedEMERGENCY LIGHTS WILL ONLY TURN OFF IN ARM, IN OFF LIGHTS STAY ONSDR CALA2020012600222Fitting · crackedSHEAR FITTING AT BS 540, LBL 6.14 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND ECRA 5714-01044.SDR CALA2020012600221Fitting · crackedSHEAR FITTING AT BS 540, LBL 15.04 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND DWG 111A2000.SDR CALA2020012600220Fitting · crackedSHEAR FITTING AT BS 540, LBL 40.87 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND ECRA 5714-01044.SDR CALA2020012600219Fitting · crackedSHEAR FITTING AT BS 540, RBL 6.14 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND DWG 111A2000.SDR CALA2020012300204Fitting · crackedSHEAR FITTING AT BS 540 RBL 15.04 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND EC / RA 57-14-01044.SDR CALA2019100501703Window Frame · crackedCRACK AT TOP OF WINDOW POST BETWEEN R-1 AND R-2 WINDOWS. NEED INSPECTION TO PERFORM HFEC ON R1 WINDOW POST FOR CRACK VERI FICATION PERFORMED HFEC PART 6 51-00-00, PROCEDURE 23, CONFIRMED EXISTING CRACK. PER AVO8019 COMPLIED WITH STEPS A1 THRU A6. PER AVO8019 SDR CALA2019093001675Windshield · crackedFO FWD WINDSHIELD CRACKED C/W STEP A THRU STEP D(2) REF AMM 56-11-11-000-0801. NEW R1 WINDOW IS DESIGNATED H13. FOUND WINDOW HEATER RESISTANCE TO BE 33.7 OHMS. MOVED TERMINAL BOARD TAP FROM TB5012 TAP 2 TO TAP 1 AMM 30-41-21-000-801 INSTALLED NEW WINDSHIELD RESDR CALA2018021900699Lens · looseL2 DOOR SLIDE COVER CLEAR VIEW BOTTLE PRESSURE LENS LOOSE. REMOVED & REPLACED L2 DOOR SLIDE ASSY, AMM REF 25-66-01-000-801 AND 25-66-01-400-801; RENDER SAFE C/L C/W; REINSTALLED CLEAR VIEW LENS ON SLIDE PACK COVER FOR SLIDE BOTTLE PRESSURE GAGE.SDR CALA2017093003353Switch · faultyEMERGENCY LIGHT SWITCH ON P5 PNL IN COCKPIT, LIGHT STAYS ON WHEN SWITCH IS IN THE ON POSITION. REMOVED AND REPLACED AFT F/A PANEL LIGHTING SWITCH REF WD 33-51- 11, OPS CHECK EMERGENCY LIGHTS REF AMM 33-51-00-720-801, OPS CHECK WORK LIGHT REF AMM 33-26-01-710-0SDR CALA2017092303307Frame · corrodedFRAME 992.8 IS CORRODED ABOVE STR 19R (MARKED). INSTALLED INTERIM REPAIR TO FRAME AT STA 992.80 ABOVE STR S-21R IN REFERENCE TO EC/RA 5310-07240.SDR CALA2017090803075Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT BS 323. REMOVED AND REPLACED.
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