N207AN
Service difficulty reports · 44
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 = 'N207AN' 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 = 'N207AN' 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 SIMA20260306001Seat Track · gougedNRWC#F106711- RH OTBD SEAT TRACK BETWEEN FRAME 23 AND 24 'IS CHAFED / GOUGED' FOUND TO BE OUT OF LIMITS. (MAJOR REPAIR) C/W REPAIR OF RH OTBD SEAT TRACK IAW ERS-EJ-53MR-5379.SDR SIMA20260303001Seat Track · corrodedDURING PASSENGER SEAT REMOVAL FOR HEAVY CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK TO BE CORRODED BETWEEN FRAMES 19-20. (MAJOR REPAIR) (LEVEL 2 CORROSION). REPAIRED SEAT TRACK IAW ERS EJ-53MR-5374.SDR SIMA20260207003Light · inoperativeRH#1 EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT INOP FAILED INSPECTION. COMPLETE:INSTALLED NEW RH#1 EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP LIGHT IAW AMM 33-50-21 OPS CHECK GOODSDR SIMA20260207004Elec Connector · disconnectedCOCKPIT EMERGENCY LIGHT INOP. REMOVED LIGHT AND FOUND TO NOT BE PLUGGED IN. REINSTALLED LIGHT IAW AMM 33-50-03, OPTS CHECK GOODSDR SIMA20251201001Battery · inoperativeEMERGENCY LIGHTS ON FWD PASSENGER DOOR WILL NOT ILLUMINATE. FOUND EMERGENCY LIGHT POWER UNIT #2 TO BE INOP. RAR EMERGENY LIGHT POWER UNIT IAW AMM 33-50-01. OPC GOOD.SDR SIMA20250927001Light · missingCCI- FOUND A PIECE OF PHOTOLUMINESCENT STRIP IN MAIN CABIN MISSING AT SEAT 4DF. OPEN.SDR SIMA20240119001Battery · inoperativeEMERGENCY LIGHT OVER ROW 12 IS OUT-C/A-RAR CABIN EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-13 AND EMERGENCY LIGHT POWER UNIT #4 IAW AMM 33-50-01 OPERATIONAL CHECK GOODSDR SIMA2024010231001Light · inoperativePORTIONS OF EMERGENCY LIGHTING FLOOR STRIP INOP-C/A-RAR PHOTOLUMINESCENT STRIP AT SEAT 3DF AND 4DF OPS CHECK GOODSDR SIMA20230428001Light · damagedALL RH AND LH EMERGENCY PHOTOLUMINESCENT FLOOR PATH STRIPS REQUIRE REPLACEMENT DUE TO FADING STRIPS AND/OR DAMAGED COVER.-C/A-COMPLETE:REPLACED ALL UNSERVICABLE LH EMERGENCY PHOTOLUMINESCENT FLOOR PATH STRIPS IAW AMM 33-50-21. REFERENCE NRWC E975733 FOR INSTALSDR SIMA20220110003None · noneO WINDSHIELD CRACKED AS WE CLIMB THROUGH 6000 FEET, RTF, NO OVERWEIGHT LANDING./ DECLARDED EMERGDENCY EQP SWAP FLT CONT. "TRANSFERRED TO NRWC 007-MIA-00911" RS 222659-C/A-REMOVED FO WINDSHEILD IAW AMM 56-11-00 STEPS 2A THRU G (10-C/A-REMOVED AND REPLACED RIGHTSDR SIMA20210828002Power Supply · inoperativeEMERGENCY LIGHTS ON AFT LH PASSENGER DOOR INOP-C/A-RAR EMERGENCY- LIGHT POWER UNIT #3 IAW 33-50-01. OPC GOOD. NO DEFECTS NOTEDSDR SIMA20201209001Engine · vibrationENGINE 2 LP VIBRATION 4.0 IN FLIGHT. C/A: PERFORMED RT ENGINE FAN BLADES AND PINS-N1 VIB TROUBLESHOOTING, IAW WORK CARD EA72-00-00-012. OPERATIONAL CHECK GOOD.SDR SIMA20201206001Battery Pack · dischargedAFT EMERGENCY LIGHTS OVERHEAD, LT OVERDOOR, AND LT LOWER INOPERABLE. C/A: ACCOMPLISHED CHARGE OF EMERGENCY LIGHT POWER SUPPLIES AND OPERATIONS CHECK GOOD, IAW AMM 33-50-01.SDR SIMA20200918002Door · vibrationFA 1 REPORTED L1 DOOR VIBRATION INFLIGHT, VIBRATION FELT AROUND DOOR AND FLOOR. STATUS PAGE SHOWED DOOR INDICATION GREEN. C/A MAIN DOOR (L1) DEFLECTOR DEFERRED, M PROC, C/W.SDR SIMA202008076001Pressure Switch · failedINBOUND FLIGHT DECLARED AN EMERGENCY FOR MECH PARKING BRAKE NOT RELEASE MESSAGE EICAS. CFR FOLLOWED FLT TO GATE, PARKING BRAKE NOT RELEASED EICAS MESSAGE ILLUMINATED. FOLLOWED FIM 32-41-00, R & R EMERGENCY BRAKE PRESSURE SWITCH SYSTEM NR 2 IAW AMM 32-44-09.SDR SIMA202007109002Door · lack of lubeMAIN CABIN DOOR DIFFICULT TO OPEN. INSPECTED AND LUBE MAIN DOOR, IAW AMM 52-11-02, OPS. CHECK GOOD.SDR SIMA2020062401003Frame · crackedFWD SERVICE DOOR LWR FWD EMERGENCY LIGHT FRAME CRACKED. REMOVED AND REPLACED THE FWD SERVICE DOOR LWR FWD EMERGENCY LIGHT FRAME IAW AMM 33-50-15-04.SDR SIMA2020061530001Slide · unknownRECORDS REVIEW STATES EMERGENCY EVACUATION SLIDE, FWD FS DOOR P/N 4A4030-7 S/N ED1922 REQUIRES RESTORATION. TRANSFERED TO DWMS NRTC E794894. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE, FWD FS DOOR P/N 4A4030-7 S/N ED1922 IAW WC 25-65-01-001-A. SEE NRTC E7SDR C77A202002170006Skin · gougedDURING BASIC CHECK AT EAMS, GOUGE DAMAGE WAS DISCOVERED ON THE LH WING FIXED
LEADING EDGE SKIN (P/N 170-31031-021) OF AIRCRAFT 207AN BETWEEN RIB 1 AND RIB 4.
REFERENCE ETD2020-170-004771-A FIGURES 1 AND 2 FOR THE DAMAGE LOCATION AND
DIMENSIONS. THE DAMAGE ESDR C77A202002170005Skin · dentedDURING BASIC CHECK AT EAMS, DENT DAMAGE WAS DISCOVERED ON THE P/N 170-61701-013 REAR FUSELAGE LOWER SKIN AT THREE LOCATIONS IN TWO BAYS BETWEEN FR94/FR95 AND S-21L/S-23L. REFERENCE ETD2020-170-005177-A FIGURE 1 FOR DAMAGE DETAILS. THE DAMAGE IS NOT ALLOWABLE PSDR C77A202002170004Skin · gougedDURING BASIC CHECK AT EAMS, GOUGE DAMAGE WAS DISCOVERED ON THE RH WING FIXED LEADING EDGE SKIN (P/N 170-31031-022) OF AIRCRAFT 207AN BETWEEN RIB 1 AND RIB 2. REFERENCE ETD2020-170-004755 FIGURES 1 AND 2 FOR THE DAMAGE LOCATION AND DIMENSIONS. THE DAMAGE EXCEEDSDR C77A202002170003Firewall · crackedDURING THE B1 BASIC CHECK IN BNA, CRACK DAMAGE WAS FOUND IN TWO LOCATIONS AT THE UPPER AND LOWER CORNERS OF THE RH APU FIREWALL REMOVABLE PANEL 351BZ (P/N 170-50263-401) ON AIRCRAFT N207AN. THE DAMAGE WAS REPAIRED PER SRM PART II 53-31-21/REPAIR 02 USING THE TSDR C77A202002170002Fitting · chafedGE LMM 78-30-00, REPAIR 017 GIVES INSTRUCTIONS TO ACCOMPLISH A REPAIR OF THE UPPER RIGHT ACTUATOR FITTING LOCATED ON THE FRONT FRAME OF THE RIGHT-HAND THRUST REVERSER HALF. THIS EO PROVIDES INSTRUCTIONS TO ACCOMPLISH SUBTASK 78-30-00-350-029, WHICH INSTALLS A SDR C77A202002170001Skin · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART II, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT RH WING TIP SPAR 1 (P/N 171-16231-002 OR 171-16231-004) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-171-22480-40SDR C77A2020021530035Seat Track · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE RH INBOARD SEAT TRACK AFT OF FR17 (P/N 170-03263-001). REFERENCE ETD2020-170-003756, FIGURE 1 FOR DETAILS, FOR THE DAMAGE LOCATION AND DIMENSION. EAMS REQUESTED & RECEIVED PERMANENTSDR C77A2020021630034Door Sill · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020021630033Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE FORWARD FUSELAGE RH IB SEAT TRACK (P/N 170-03263-001) BETWEEN FR13 AND FR14 IN THE FORWARD CABIN FLOOR STRUCTURE. SDR C77A2020021530032Splice · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020021530031Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020021530030Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020021530029Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A202002153028Shear Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020021503027Shear Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830026Splice · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830025Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830024Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830023Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830022Shear Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020300021Shear Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830020Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-65928-001 CENTER SHEAR PANEL, P/N 170SDR C77A2020020830019Seat Track · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE RH INBOARD SEAT TRACK AFT OF FR17 (P/N 170-03263-001). REFERENCE ETD2020-170-003756, FIGURE 1 FOR DETAILS, FOR THE DAMAGE LOCATION AND DIMENSION. EAMS REQUESTED & RECEIVED PERMANENTSDR C77A2020020700041Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE FORWARD FUSELAGE RH IB SEAT TRACK (P/N 170-03263-001) BETWEEN FR13 AND FR14 IN THE FORWARD CABIN FLOOR STRUCTURE. SDR C77A2019071000001Strut · lack of lubeLG WOW SYS FAIL. PERFORMED NLG SHOCK STRUT SERVICING IAW AMM 12-12-09. DURING RELEASE OF NITROGEN AND HYDRAULIC FLUID, FOUND NO FLUID IN NLG SHOCK STRUT. WO REMAINS OPEN. GEAR SWING REQUIRED. PERFORMED FUNCTIONAL TEST OF THE LG EXTENSION AND RETRACTION SYSTEM SDR C77A20170124002Unknown · smokeFLIGHT RETURNED TO DEPARTURE DUE TO REPORTED SMOKE AND BURNING ODOR IN THE CABIN AFTER TAKE OFF BELOW 1000 FEET. . REPORTS INDICATE THAT THE SUSPECTED SMOKE DISSIPATED AND HAS NOT CAUSED ANY ISSUES. AN EMERGENCY WAS DECLARED. LANDED SAFELY WITHOUT INCIDENT. P
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