N7750A
Service difficulty reports · 257
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 = 'N7750A' 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 = 'N7750A' 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 SWAA2025122234830Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 192HR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 192HR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025122234831Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 192AR BODY FAIRING AT FUSELAGE EXTERIOR . REPAIRED ACCESS PANEL 192AR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025122234826Access Panel · elongatedELONGATED HOLE ACCESS PANEL 192AL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 192AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-9 REPAIR 9.SDR SWAA2025122234662Plate · deterioratedDETERIORATED HARDWARE OF GIRT BAR FITTING AND ADAPTER PLATE AT AFT SERVICE DOOR. EPLACED HARDWARE OF GIRT BAR FITTING AND ADAPTER PLATE AT AFT SERVICE DOOR IAW AMM 25-66-02-400-801 FOR INSTALLATION STEPS SEE TASK 725-025-00-02Y.SDR SWAA2025122254801Fitting · deterioratedDETERIORATED HARDWARE OF GIRT BAR FITTING AND ADAPTER PLATE AT AFT SERVICE DOOR. REPLACED HARDWARE OF GIRT BAR FITTING AND ADAPTER PLATE AT AFT SERVICE DOOR IAW AMM 25-66-02-400-801 FOR INSTALLATION STEPS SEE TASK 725-025-00-02Y.SDR SWAA2025121935041Support Angle · crackedCRACKED CEILING AREA, CARGO LINER SUPPORT ANGLE ON BS 827 LT SIDE IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ANGLE, BTW BS 807 - 847 IAW SRM 51-70-11-2R-0, REPAIR GENERAL, FIGURE 202, SHEET 2, AND DETAIL B.SDR SWAA2025121934661Fitting · deterioratedDETERIORATED HARDWARE OF GIRT BAR FITTING AND ADAPTER PLATE AT AFT ENTRY DOOR. REPLACED HARDWARE OF GIRT BAR FITTING AND ADAPTER PLATE AT AFT ENTRY DOOR IAW AMM 25-66-02-400-801 FOR INSTALLATION STEPS SEE TASK 725-025-00-02Y, TTG8Q002EMLT. STEP 13.SDR SWAA2025122234469Access Panel · crackedCRACKED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2025121934313Plate · corrodedCORRODED PLATE, FLOOR PANEL 140CF BS 807, RT SIDE AT AFT CARGO BAY. REPLACED THE PLATE IAW SRM 51-40-02.SDR SWAA2025121934463Gusset · crackedCRACK GUSSET LOCATED AT, BS 500D, FWD CARGO BAY. REPLACED GUSSET AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET, 209, REV - .SDR SWAA2025121934466Gusset · crackedCRACKED GUSSET, BS 500D, STR 19R IN THE FWD CARGO BAY. REPLACED GUSSET AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 209, REV -.SDR SWAA2025122234296Strip · deterioratedDETERIORATED PHOTOLUMINESCENT LT & RT SIDES IN THE PASSENGER CABIN (10EA). REPLACED PHOTOLUMINESCENT STRIPS IAW AMM 33-51-15-400-802.SDR SWAA2025110732216Skin · delaminatedLEFT WING OTBD AFT FLAP, INBD LOWER CORNER DELAMINATED ON TOP SKIN WHICH MEASURES 13 X 8 AND BOTTOM SKIN WHICH MEASURES 9 X 5. BOTH SURFACE SKIN EDGES ARE NOT DELAMINATED IAW EA 25-127-03054.SDR SWAA2025063084750Seat Back · out of adjustPASSENGER CABIN SEAT 11B RECLINES SLIGHTLY AND; AS IT IS IN AN EMERGENCY EXIT ROW; IS NOT SUPPOSED TO. IT SHOULD BE LOCKED OUT TO PREVENT RECLINING. <[01] SECURED PASSENGER CABIN SEAT RECLINE IN LOCKED POSITION AT SEAT 11B IN REF CMM 25-21-45.SDR SWAA2025041423334Sign · intermittentOVERWING EMERGENCY EXIT SIGN FLICKERS ON/OFF INTERMITTENTLY WHEN ARMED.<[01] PERFORMED EMERGENCY LIGHT OPERATIONAL CHECK REF AMM 33-51-00. OPS CHECK GOOD.SDR SWAA2025020492661Seat · looseSEAT ROWS ARE LOOSE IN TRACK AT SEAT ROWS 13 ABC AND 14 DEF.<[01] TIGHTENED SEAT MOUNTING HARDWARE PER AMM 25-22-00.SDR SWAA2024100143098Slide · out of adjustR2 WINDOW UPPER REAR NUT MISSING ON SLIDE<[01] REPLACED MISSING NUT; WASHER; AND SPACER AT F/OS SLIDING WINDOW UPPER HOUSING IAW AMM 56-12-11-220-001; OPS CHECK GOOD.SDR SWAA2024091637223Lens · looseR1 DOOR EMERGENCY SLIDE GAUGE LENS LOOSE<[01] RESECURED R1 DOOR EMERGENCY SLIDE WINDOW REF M/M 25-66-01SDR SWAA2024080622094Lamp · inoperativeL2 EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW AMM 33-51-04 OPERATION CHECKS GOOD AT THIS TIME.SDR SWAA2024041172390Light · inoperativeEXTERIOR EMERGENCY LIGHTS INOP. AT AFT SEVICE DOOR AND JUST FWD OF AFT CARGO DOOR.<[01] RELAMPED EXTERIOR EMERGENCY LIGHTS AT AFT SERVICE DOOR AND AFT CARGO DOOR IAW AMM 33-51-04.SDR SWAA2024040570916Generator · faultyFOR 2 OR 3 MIN ON DECENT AN ELECTRICAL ARCING SOUND EMINATED FROM THE OVERHEAD PANEL IN THE VICINITY OF THE FUEL & BUS TRANSFER PANELS. NO STATIC ELECTRICITY NO STATIC AND VISIBLE ON WINDOWS. OZONE SMELL NO ACCOMPANY SOUND<[01] C/W SMOKE/FUMES IN CABIN CONDITISDR SWAA2024040570941Module · arcedFOR 2 OR 3 MIN ON DECENT AN ELECTRICAL ARCING SOUND EMINATED FROM THE OVERHEAD PANEL IN THE VICINITY OF THE FUEL & BUS TRANSFER PANELS. NO STATIC ELECTRICITY NO STATIC AND VISIBLE ON WINDOWS. OZONE SMELL NO ACCOMPANY SOUND<[01] C/W SMOKE/FUMES IN CABIN CONDITISDR SWAA2023122130231Battery Pack · inoperativeEMERGENCY LIGHTS COMMON TO BATTERY M1670 INOP REFERENCE WDM 33-51-13 FOR SPECIFIC INOP LIGHTS<[01] VERIFIED MEASUREMENTS TABLE.;[02] REMOVED; REPLACED AND PERFORMED GOOD OPS TEST OF M1670 BATTERY PACK AS DOCUMENTED ON ASSOCIATED STEPS.SDR SWAA2023122129844Handle · damagedPASSENGER CABIN FWD ENTRY DOOR SIDEWALL PANEL AFT SIDE DAMAGED AT ASSIST HANDLE HOLE<[01] REPAIRED PASSENGER CABIN ENTRY DOOR SIDEWALL PANEL AFT SIDE ASSIST HANDLE HOLE IAW CMM 25-00-66; REPAIR 3-1; PAGES 603-604 SECTION 4. C.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023122128505Tee Angle · crackedT-CLIP P/N 149A7627-5 COMMON TO BS 663 VAPOR BARRIER WL 150 LBL 25 IS CRACKED<[01] REMOVED AND REPLACED PER REF SRM 51-40-02 AND DWG 111A7000;[02] VERIFIED CORRECTIVE ACTIONS STEP 1 AND MEASUREMENTS TABLE.SDR SWAA2023122126408Angle · crackedANGLE P/N 149A7218-7 BS 649-663; WL 142-150; LBL 25 IS CRACKED<[01] REMOVED AND REPLACED PER REF SRM 51-40-02 AND DWG 111A7000;[02] VERIFIED CORRECTIVE ACTIONS STEP 1 AND MEASUREMENTS TABLE.SDR SWAA2023122125969Floor Panel · pulledAFT FLOOR PANEL 241ACF HAS PULLED THROUGH INSERT<[01] FLOORBOARD 241ACF THROUGH INSERT REPAIR HAS BEEN FINISHED IAW SRM 53-00-50-2R-6.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 241ACF REPAIR HAS BEEN PERFORMED SRM 53-00-50-2R-6.SDR SWAA2023122125362Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOORBOARD 222BF UPPER SKIN HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 222BF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[03] WORSDR SWAA2023122125365Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB SDR SWAA2023122125366Floor Panel · pulledFWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXCESSIVE DAMAGE FWD FLOOR PANEL 232BF WAS REPLACED WITH A NEW SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125351Floor Panel · pulledPANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241WF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125352Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242AF WAS REPLACED WITH NEW SERVICEABLE PANEL IAW SRM 51-10-01-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125355Floor Panel · pulledPANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242QF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125357Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FWD FLOOR PANEL 221CF WAS REPLACED WITH A NEW SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PAR 9.A.(1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125360Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 221DF PER IS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2023122125346Floor Panel · pulledPANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231ZF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125347Floor Panel · pulledPANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 232SF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIESDR SWAA2023122125348Floor Panel · pulledPANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0127.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.SDR SWAA2023122125349Floor Panel · pulledPANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241BF WAS REPLACED WITH NEW SERVICEABLE PANEL IAW SRM 51-10-01-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125350Floor Panel · pulledPANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0470.;[02] ATTACHED CURE SHEET.<BR>SDR SWAA2023122125354Floor Panel · pulledPANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125340Floor Panel · crackedAFT FLOOR PANEL 242WF O/B AFT CORNER IS CRACKED.<[01] REPAIRED DAMAGED O/B AFT CORNER ON AFT FLOOR PANEL 242WF IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.SDR SWAA2023122125343Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242SF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.;[02] PANEL REPLACED. JOB COMPSDR SWAA2023122125344Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] VERIFIED COMPLETION OF REPAIR TO AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1;[02] VERIFIED REPAIR OF AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1;[03] WORKSCOPE IS COMPLETE.SDR SWAA2023122125345Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS.;[02] AL STEPS COMPLETESDR SWAA2023122125353Floor Panel · pulledPANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125337Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXCESSIVE DAMAGE AFT FLOOR PANEL 241ABF WAS REPLACED WITH A NEW SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125338Floor Panel · pulledAFT FLOOR PANEL 241ADFF UPPER SKIN HAS AREAS OF PULLED STRANDS. CORRECT PANEL IS 241ADF.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGSDR SWAA2023122125339Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242RF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB SDR SWAA2023122125342Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOORBOARD 241ACF UPPER SKIN HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 241ACF UPPER SKIN HAS BEEN REPAIRED PER SRM 53-00-50-
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