N8520Q
Service difficulty reports · 78
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 = 'N8520Q' 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 = 'N8520Q' 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 SWAA2026081365334Flashlight · failedCAPTAIN`S SIDE AFT FLIGHT ATTENDANT FLASHLIGHT WOULD NOT TEST. R & R AFT INBD EMERGENCY FLASHLIGHT BATTERY AND TAMPER SEAL. OPS CHKD GOOD IAW AMM 25-64-00.SDR SWAA2026071532933Bushing · corrodedRIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG, OUTER FACE HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED ALL 4 RT MLG FWD TRUNNION BUSHINGS IAW AMM 20-10-02, ALSO REF. E. A. 1-A57-3246. LT OR RR MLG FORWARD TRUNNION FITTING LUG CORROSION REPAIR. RSDR SWAA2026062515497Light · inoperativeLEFT OVERWING EXIT AFT EMERGENCY LIGHT IS INOPERATIVE. GOOD OPERATIONAL TEST OF EMERGENCY LIGHTS PER AMM 33-51-00-710-801. LT OVERWING EXIT AFT LIGHT OPERATIONAL.SDR SWAA2026062514712Fuse · inoperativeFWD SERVICE DOOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE SUSPECT FUSE BAD. CHANGED FUSE ON (M2816) AND PERFORMED A GOOD TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-06-960-804. OPS CHECK GOOD.SDR SWAA2026051898273Unknown · odorJUST PRIOR TO LANDING; BOTH FLIGHT ATTENDANTS IN AFT JUMP SEAT; FOS SIDE SMELLED A STRONG SMOKE SMELL; DISSIPATED AT GATE WHEN DOOR OPENED<[01] PREFORMED BIRD STRIKE INSPECTION PER AMM 05-51-18 AND A SMOKE OR FUMES IN CABIN PER AMM 05-51-56. FOUND NO EVIDENCE SDR SWAA2026032380941Latch · looseFWD SERVICE DOOR EMERGENCY SLIDE CAME OUT OF DOOR COVER. R & R SECURING LATCH ON FWD SERVICE DOOR EMERGENCY SLIDE; RE-INSTALLED FWD SRV DOOR EMERGENCY SLIDE REF AMM 25-66-01. REF LP# 3031454 FOR SLIDE REMOVAL. NO FURTHER DEFECTS NOTED AT THIS TIME. EMERGENCYSDR SWAA2026032380942Slide · dislodgedREF L/P# 3031453 FWD SERVICE DOOR EMERGENCY SLIDE CAME OUT OF DOOR COVER<[01] REMOVED FWD SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01SDR SWAA2026021971874Slide · unsecureFWD ENTRY DOOR SLIDE HANGING OUT. SECURED THE SLIDE IAW MT 725-61-06.SDR SWAA2026012864555Actuator · out of adjustSEAT 13D RECLINES INTO EXIT ROW. ADJUSTED THE ACTUATOR IAW MM S.I.P.SDR SWAA2025112036060Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1695 WILL NOT HOLD CHARGE. REMOVED & REPLACED THE BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.SDR SWAA2025112034118Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231UF HAS FIBERS MISSING AND PULLING LOOSE IN MULTIPLE AREAS ON UPPER SURFACE. REPAIRED PASSENGER CABIN FLOOR PANEL 231 UF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.SDR SWAA2025112032832Floorbeam · crackedMID CABIN FLOOR EXPANSION JOINT AT BS 540 CRACKED AT FASTENER LOCATION NEAR LBL 1. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, SHEET 64, REV -. APPLIED CIC IAW AMM 51-21-91-620-802.SDR SWAA2025112032831Floorbeam · crackedMID CABIN FLOOR EXPANSION JOINT AT BS 540 CRACKED AT FASTENER LOCATION NEAR RBL 1. REMOVED AND REPLACED THE FLOORBEAM ASSY IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, SHEET 64, REV- APPLIED CIC IAW AMM 51-21-91-620-802.SDR SWAA2025112032385Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242BF HAS PULLED FIBERS ON TOP SIDE. REPAIRED PASSENGER CABIN FLOOR PANEL 242BF ON UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.SDR SWAA2025112032386Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231ZF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 231ZF REPAIRED IAW SRM 53-00-50-2R-1 AND EA M-25-153-02385.SDR SWAA2025112032387Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231YF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 231YF REPAIRED IAW SRM 53-00-50-2R-1 AND EA M-25-153-02385.SDR SWAA2025112032388Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 241AF REPAIRED IAW SRM 53-00-50-2R-1, AND EA M-25-153-02385.SDR SWAA2025112032389Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241DF HAS PULLED FIBERS ON TOP SIDE. FLOOR PANEL 241DF REPAIRED IAW SRM 53-00-50-2R-1 AND EA M-25-153-02385.SDR SWAA2025081403939Flashlight · inoperativeAFTER GALLEY FLIASHLIGHT ON FOS SIDE INOPERATIVE. REMOVED AND REPLACED BATTERY PER AMM 25-64-00.SDR SWAA2025062785442Battery Pack · inoperativeFWD FA FLASHLIGHT IS INOP FWD FLIGHT ATTENDANT FLASH LIGHT IS INOP<[01] REMOVED AND REPLACED BATTERY PER AMM 25-64-00.SDR SWAA2025060276198Light · inoperativeL2 DOOR EXTERIOR EMER LIGHT INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801- NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)].SDR SWAA2025042126513Flap System · lockedON APPROACH; FLAP HANDLE WAS AT 15; FLAP TRAILING EDGE INDICATED LEFT 10; RIGHT TRAILING EDGE INDICATED 5. ON GO AROUND; BOTH TRAILING EDGE FLAPS INDICATED 10. QRH DIRECTED ALTERNATE FLAP (CONTINUED) USAGE TO FLAPS 15. NORMAL BRAKING USED. AUTO BRAKE 3. NORMALSDR SWAA2025031705287Sign · out of adjustR/H OVERWING EMER EXIT LIGHT/SIGN FELL OFF <[01]. INSTALLED NEW EMER EXIT LIGHT/SIGN AMM 33-51-01.SDR SWAA2025022196872Engine · leakingBEGAN WITH 87% OIL QUANTITY ON ENGINE #2. AFTER TAKEOFF IT WENT TO 1% WITH WHITE BOX. AFTER REDUCING THRUST OIL QUANTITY INCREASED TO 15% TO 30%. WHEN ON GROUND WHEN INCREASING THRUST OIL QUANTITY DROPS SIGNIFICANTLY. PERFORMED #2 ENGINE EXTERNAL OIL SYSTEM SDR SWAA2024111858261Angle · crackedLEFT AIR CONDITIONING COMPARTMENT UPPER INBD L ANGLE AT STA 663 POSSIBLE CRACK PHOTO ATTACHED<[01] ACCOMPLISHED HFEC SURFACE INSPECTION PER NDT PART 6 51-00-00 PROC. 23 OF SUSPECT AREA VERIFIED ANGLE IS CRACKED.;[02] CRACK LENGTH IS .200';[03] CRACK LOCATED INSDR SWAA2024111858262Angle · crackedRIGHT AIR CONDITIONING COMPARTMENT UPPER INBD L ANGLE AT STA 663 POSSIBLE CRACK PHOTO ATTACHED<[01] ACCOMPLISHED HFEC SURFACE INSPECTION PER NDT PART 6 51-00-00 PROC. 23 OF SUSPECT AREA VERIFIED ANGLE IS CRACKED.;[02] CRACK LENGTH IS .700';[09] FABRICATED REPASDR SWAA2024111857585Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK AT STA 527C R/H IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION.SDR SWAA2024111857583Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK AT STA 565 LEFT OVERWING IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION.SDR SWAA2024111857584Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK AT STA 727C L/H IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION.SDR SWAA2024111854682Floor Panel · debondedPNL 231XF HAS DISBONDED AND EXPOSED FIBERS<[01] R+R'D FLOOR PANEL 231XF. REF AMM 53-21-00;[02] GRANTED : OK TO INSTALLED;[03] VERIFIED C/A # 1 : YOSVANYS LEMAS SANTO (TECHNICIAN); 29-OCT-2024 23:20 UTC<BR>R+R'D FLOOR PANEL 231XF. REF AMM 53-21-00SDR SWAA2024111854683Floor Panel · debondedPNL 241AF HAS DISBONDED AND EXPOSED FIBERS<[01] R+R'D FLOOR PANEL 241AF. REF AMM 53-21-00;[02] GRANTED : OK TO INSTALLED;[03] VERIFIED C/A # 1 : YOSVANYS LEMAS SANTO (TECHNICIAN); 29-OCT-2024 23:18 UTC<BR>R+R'D FLOOR PANEL 241AF. REF AMM 53-21-00SDR SWAA2024111852739Floor Panel · corrodedFWD CARGO FLOOR PANEL HAS CORROSION ALONG AFT EDGE; 120DF.<[01] R/R FWD CARGO FLOOR PANEL 120DF REF. AMM 25-52-10.;[02] INSPECTED WORK PERFORMED. R/R FWD CARGO FLOOR PANEL 120DF REF. AMM 25-52-10.SDR SWAA2024111852516Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727H-727I AROUND FASTENER HOLES.<[01] MEASURED CORROSION DAMAGE AT AFT CARGO LEFT SIDE SUPPORT ZEE STATION 727H TO 727I; ORIGINAL THICKNESS IS .040?; DAMAGE DEPTH IS .006? ATSDR SWAA2024111852482Scuff Plate · crackedFORWARD CARGO FORWARD CORNER SCUFF PLATE IS CRACKED.<[01] OK TO INSTALL;[02] REPLACED FORWARD CARGO FORWARD CORNER SCUFF PLATE PER AMM 53-11-02-420-801SDR SWAA2024111852483Scuff Plate · crackedFORWARD CARGO AFT CORNER SCUFF PLATE IS CRACKED<[01] OK TO INSTALL;[02] REPLACED FORWARD CARGO AFT CORNER SCUFF PLATE PER AMM 53-11-02-420-801SDR SWAA2024111851595Bracket · crackedAPU FEEDER CABLE SUPPORT BRACKET CRACKED STA 867 RBL 18 WL300<[01] FABRICATED FEEDER CABLE SUPPORT BRACKET; P/N 287A4015-9; PER BOEING DRAWING #287A4015 AND SMAL - BOEING CONTROL NUMBER 0271023258.;[02] VERIFIED. FABRICATED FEEDER CABLE SUPPORT BRACKET; P/N 28SDR SWAA2024111851589Angle · crackedCRACK IN FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 RBL 10<[01] REMOVED CRACK FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 RBL 10.<BR>LOCATED; DRILLED AND INSTALLED NEW FLOOR BEAM WEB ALL WORK REFERENCE 51-40-02;[02] INSPECTED WORK ABOVESDR SWAA2024111851590Angle · crackedCRACK IN FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 LBL 13<[01] REMOVED CRACK FLOOR BEAM WEB ANGLE BETWEEN STA. 380-400 LBL 13.<BR>LOCATED; DRILLED AND INSTALLED NEW FLOOR BEAM WEB ALL WORK REFERENCE 51-40-02;[02] INSPECTED WORK ABOVESDR SWAA2024050983388Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS WILL NOT ILLUMINATE THROUGHOUT THE AIRCRAFT<[01] REMOVED AND REPLACED BATTERY PACKS AT THE FOLLOWING POSITIONS; M1671;M1672;M1675 AND M2335 PER AMM 33-51-06SDR SWAA2024021552174Megaphone · intermittentFWD MEGAPHONE INTERMITTENT<[01] R AND R FWD MEGAPHONE AND OPS CK OK. REF AMM 25-64-00. BATTERY EXP JUN 2025SDR SWAA2023122734968Sign · inoperativeFWD RH EXTERIOR EMERGENCY LIGHT AND FWD OVER DOOR EXIT SIGN LIGHT INOP<[01] REMOVED AND REPLACED APPLICABLE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOODSDR SWAA2023121330379Flashlight · inoperativeAFT LEFT FLASHLIGHT INOP<[01] R/R AFT LEFT FLASHLIGHT BATTERY PER AMM 25-64-00SDR SWAA2022111467800Web · crackedRH WING PNL SUPPORT WEB CRACKED. RH WING PNL SUPPORT WEB CRACKED JUST INBD OF DEFLECTION CONTROL RIB. REMOVED AND REPLACED DAMAGED SUPPORT WEB PER SRM 51-40-02.SDR SWAA2022111466145Floor Panel · damagedCABIN FLOOR PANEL 231XF HAS MULTIPLE FIBERS EXPOSED. / [01] REMOVE AND REPLACED FLOOR BOARD PER AMM 53-21-00.;[02] REMOVE AND REPLACED FLOOR BOARD PER AMM 53-21-00.<BR>PART INFORMATION NEEDED.SDR SWAA2022111465874Floor Support · corrodedFLOOR SUPPORT BETWEEN STA 747 AND 767 RBL 21 HAS CORROSION AROUND NUTPLATE HOLES. LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02.SDR SWAA2022111465875Angle · damagedFWD CARGO, LT TRANSITIONAL ANGLE AT BS 500B+8 THRU 500G+10, WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE SECTION IAW SRM 51-40-02. LOCATED AND DRILLED FWD SPICE AT BS 500B +9 IAW SRM 53-00-53-2R-5. REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-1SDR SWAA2022111464974Angle · corrodedTHE AFT CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 770 TO 774 / [01] FOUND CORROSION ON R/H SIDE PLATE FROM STA 767-792 TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED SHIELD; MATCH DRILLED NEW SHIELD PER SRM 51-40-05;[03] INSP DRILLINSDR SWAA2022111464975Angle · corrodedTHE AFT CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 727H +8 TO 767, FOUND TO BE OUT OF LIMITS IAW SRM 53-0053-1A-2. REMOVED DAMAGED SECTION OF RT TRANSITION ANGLE IAW SRM 53-00-53-2R-5. LOCATED, DRILLED, TREATED AND PRIMED. IAW SRM 53-00-53-2R-5. INSTASDR SWAA2022111464976Angle · corrodedTHE AFT CARGO L/H TRANSITION ANGLE HAS CORROSION FROM STA 727F+10 TO 807 / LT TRANSITION ANGLE UPPER SURFACE FORM STA 727I TO STA 807; LBL 21; WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION OF LT SIDEPLATE CHANNEL ASSEMSDR SWAA2022111465420Angle · corrodedRIGHT TRANSITION ANGLE; STA. 500A THRU 500I CORRODED, FOUND OUT OF LIMITS. LOCATED AND DRILLED NEW IAW SRM 51-40-02. REPLACED THE RH SIDE TRANSITION ANGLE IAW SRM 51-40-02.
Back to N8520Q