N57868
Service difficulty reports · 108
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 = 'N57868' 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 = 'N57868' 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 CALA2024121101474Seal · dirtyLOUD HUMMING VIBRATION EMANATING FROM TOP OF EXIT DOOR AT 22F RE PORTED BY PILOT UA CAPTAIN WHO WAS SEATED AT 22F REPORTED CONSTANT BUZZING NOISE AT THE TOP OF THE AFT HATCH DOOR THRU OUT FLIGHT THAT CAN BE HEARD FROM THE COCKPIT TO AFT GALLEY. PRESSURIZED CABSDR CALA2024110501020Hose · faultyAFTER GEAR RETRACTION GEAR DOORS EICAS CAUTION FLOOR VIBRATION M IDCABIN 2.5 UNITS LEFT RUD TRIM PSEU LAST LEG FAULT RECALL LISTED RIGHT GEAR DOOR CLOSED SENSORS S10241 (SYS 1) AND S10072 (SYS 2), MAINT MSGS 32-61142 & 32-61139, NEEDS FURTHER T-S. FOUND RT MLGSDR CALA2024102400916Bezel · misinstalledR EMERGENCY EXIT WINDOW BEGAN RATTLING ON DESCEN T AT 36000 FT. FOUND BEZEL IN PLACE BUT UPSIDE DOWN. RETURNED TO CORRECT POSITION. BEZEL IS SECURE.SDR CALA2024032500855Skin · crackedLEFT WING FIXED LEADING EDDGE ABOVE THE PYLON IS CRACKED. PART IS CURRENTLY RMOVED FROM THE AIRCRAFT.SDR CALA2024032500854Panel · crackedGEN ITEM; EA 5720-03041 REV E OP 006/// NO 2 ENGINE PYLON TO WIN G LEADING EDGE PANEL ASSEMBLY CRACKED. PANEL ASSEMBLY IS CURRENT LY REMOVED FROM THE AIRCRAFT. REPORTED BY V932161SDR CALA2024032100803Unknown · crackedGEN ITEM; EA 5310-07582 REV A OP 003 7837 A STRINGER CLIP IS CRACKED. LOCATED AT THE FWD SIDE OF B STA FRAME1460 S-26L REPORT ED BY V921214 REMOVED & REPLACED STRINGER CLIP FLOOR SUPPORT IN THE ALC AT STA 1460 LEFT SIDE IAW B757 SRM 51-40-02 PARA 7. SEE BACK FSDR CALA2024031500736Floor Panel · crackedREF AMES NR 169356-0100-0067 GENERATING ITEM: 53-5330-1-2802///A FT LOWER CARGO HAS 6 INCH CRACK APPROXIMATELY IN FIXED FLOOR PAN EL IN-BETWEEN STATIONS 1280-1300 JUST ABOVE STRINGERS S-26R, MAR KED WITH STREAMER 3254 INSTALLED REPAIR DOUBLE ON THE ALC TRANSISDR CALA2023071202230Spoiler · unknownRUDDER TRIM EXCESSIVE LEFT IN FLIGHT CRUISE. A/C SETTLED AROUND 9 DEGREES IN CRUISE. NO VIBRATIONS NOTED DURING FLIGHT. A/C SLIGHT LEFT ROLL ON TAKEOFF. PILOTS NOTICED HAVING TO ADD T/S PER FIM 27-21 FAULT TREE 812 UPTO BLOCK 33 RECONNECTED RT C/W FIM 27-21-00SDR CALA2022093002563Skin · noneSUPPORT TASK RH HORIZONTAL STAB UPPER EXTERIOR SURFACE HAS 1 EA EXISTING REINFORCING REPAIR APRPOX 78 IN. OTBD OF THE INBD EDGE OF THE STAB TO THE CENTER OF THE REPAIR MEASURING APPROX 5.5 IN. X 5.5 IN. SQUARE BETWEEN THE AUX SPAR AND THE FWD SPAR. REPAIR APPESDR CALA2022090202235Engine · noneTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/02/22. COMRESSOR STALL RIGHT ENGINE CLIMBING THROUGH 9000. #2 ENG REPLACED.SDR CALA2021110302019Seal · missingPDA 2 RIGHT WING OUTBD MAIN T/EDGE FLAP COMPLETELY MISSING SEAL AT INBOARD END (WHERE INBOARD & OUTBD FLAPS MEET) -- SEE PHOTO PHOTO ADDED PHOTO - SEAL MISSING 42" LONG -- SDR REQUIRED PER GMM 02-30-95 INSTALLED & SECURED NEW SEAL AT INBOARD END OF RIGHT WING SDR CALA2021051000631Service Panel · corrodedB757-06-3-2222 EVIDENCE OF CORROSION FOUND AFT OF LAV SERVICE PA NEL (AREA MARKED) REF HAECO GSO NR LP 9282246 PERFORM AN INSPECTION PER PART 2 OF ECRA 5361--01083 ON OR BEFORE 62,200 TOTAL AIRCRAFT FLIGHT CYCLES. EC/RA 5361-0183, PERFORM AN INSPECTION PER PARSDR CALA2021043000566Skin · dentedREF LP 1451835 & 4152113 WHILE ACFT WAS IN LAS - RAMP REPORTED D ENT LEFT SIDE OF FUSELAGE FWD OF L2 DOOR. LASMM LOCATED AND MEAS URED DENT. DENT IS LOCATED AT STA 574 BETWEEN STR 19L & 20L. DEPTH MEASURES .025 WIDTH 0900. PER SRM 53-00-01 ALLOWABLE DAMAGE FISDR CALA2021042800563Skin · dentedREF LOG 4160847 DENT LOCATED AT STA 574 BETWEEN STR 19L & 20L CARRIED AS DMG, RE-INSPECTION REQUIRED HAECO/GSO LOG 9283059, V900838 REEVALUATED DENT AT STA 754 BETWEEN STR 19L & 20L, DENT FOUND TO BE OUT OF LIMITS HAECO LOG 9283059, V900838 REPAIRED DENT AT STSDR CALA2021042200512Seat Track · corrodedB757-53-3-0480: I/B SEAT TRACK HAS EVIDENCE OF CORROSION BTWN BS 1300 AND 1320 ON RBL24. REF HAECO GSO NR 9282683 BLENDED CORROSION PER B757 SRM 53-00-52 AND FOUND TO BE OUT OF L IMITS. REMOVED SEAT TRACK IAW B757 SRM 53-00-52 R1. MACHINED 1EA REPAIR SEAT TRASDR CALA2021041400460Fitting · damaged(SUPPORT TASK) MAIN CABIN STA1329 RBL24 SEAT TRACK FITTING HAS UNFINISHED DRILLED HOLE IN RADIUS. REF HAECO GSO NR # 9283265. REMOVED FLOOR PANELS 252EF AND 251JF IAW B757-300 AMM 53-01-01- 024-022. REMOVED DAMAGED FITTING AT STA 1329 RBL24 IAW B757-300 SRM 51SDR CALA2021041400459Cusp Web · gougedB757-53-3-0480: R/H CUSP BS644 S17R LWR SURFACE HAS CIRCULAR GOU GE. REF HAECO GSO NR 9282773 ACCOMPLISHED BLEND ON RH CREASE BEAM WEB BS644 S17 AND DETERMINE D DAMAGE TO BE OUT OF LIMITS IAW B757 SRM 53-30-15 AND BDWG 143N 5520. ORIG THICKNESS .050", DEPTH OSDR CALA2021041400458Frame · crackedB757-53-3-0555: FRAME 310.5 CRACKED AT S4L. REF HAECO GSO NR 92 82742 PERFORMED DAMAGE REMOVAL IAW HAECO REO-G23005 STAGE 1 STEP 5. PE RFORMED HFEC INSP OF CUTOUT, NO FURTHER DAMAGE NOTED. PERFORMED .040 CUT PER HAECO REO-G23005, STAGE 1 STEP 7. ACCOMP DVI OFSDR CALA2021040500414Floorbeam · corrodedB757-53-3-0575: MAIN CABIN FLOOR STRUCTURE DECK PLATE CORRODED A T STA 1681 BTWN LBL 24.75 AND LBL 45.50. REF HAECO GSO NR 92827 00 REMOVED CORROSION IAW B757 SRM 51-10-02. ORIG THICKNESS .071, RE MOVED .043, REMAINING .028 IS NOT WITHIN ALLOWABLE LIMITS IAW SDR CALA2021040500416Seat Track · gougedB757-57-3-0006: SEAT TRACK GOUGED UPPER SURFACE BS 1120-BS 1140, LBL24. REMOVED AND REPLACED MAIN CABIN SEAT TRACK SECTION FROM STA 1075 -1180 LBL24 P/N 114N5021-4 IAW BAC DWG 144N5021 REV C, 144N5001 REV A, 144N5260 REV B, B757 SRM 51-40-02, SRM 51-40-05, SSDR CALA2021040500415Seat Track · gougedB757-57-3-0006: SEAT TRACK GOUGED UPPER SURFACE BS 1120-BS 1140 LBL45. REMOVED AND REPLACED MAIN CABIN SEAT TRACK SECTION FROM STA 1075 -1180 LBL45 P/N 144N5021-4 IAW BAC DWG 144N5021 REVC, 144N5001 R EVA, 144N5260 REVB, B757 SRM 51-40-02, SRM 51-40-05, SRM 5SDR CALA2020051100953Skin · dentedDENT REPORTED TO SM FRONT OF L2 DOOR. LOCATION IS STA 612 STR 16 L. DENT MEASURES 2.2"X2.8"X.120" A/Y IS 18.3 AND IS OUT OF LIMITS AND MUST BE REPAIRED, THE REPAIR MAY BE DELAYED SINCE ALL OTHER CRITERIA IS WITHIN LIMITS PER 757-3 SRM 53-00-01 NOTE I. INITIATESDR CALA2019072401236Idg · inoperativeL GEN KICKED OFF INFLGHT FOLLOWED QRH. RESET ONCE KICKED OFF AGAIN. REMOVE THE CONNECTOR BACKSHELL AND INSPECT THE WIRES IF THE ABOVE LOOKS GOOD, THEN DISCONNECT D1014P AT THE PYLON DISCONNECT AND INSPECT CONTACTS 3,12,13 AND 14 FOR DAMAGE NECTOR AND INSPECT TSDR CALA2019050300684Unknown · malfunctionedHF RADIOS BOTH INOP UNREADABLE. PLACED ITEM ON MEL 2311AK. BOTH HF ARE INOP. COMPLIED WITH MEL. PER FIM TASK 23-11-00-815-802 BOTH HF1 AND HF2 GOOD. CALLED SFO HF 1 & HF2 GOOD TX AND RCV.SDR CALA2018021800683Lamp · inoperativeEMERGENCY LIGHTS UNARMED INDICATOR HAS ONE LAMP INOPERATIVE ON OVERHEAD PANEL. REPLACED THE LAMP IAW MM 33-11-00SDR CALA2018010700090Light · inoperativeSLIDE LIGHT DOOR 2R NEEDS RELAMP. RELAMPED 2R DOOR SLIDE LIGHT. OPS CHECK GOOD.SDR CALA2017123104713Sign · looseDOOR 2 EMERGENCY EXIT SIGN HANGING LOOSELY SECURED EXIT ROW SIGN, OPS NORMAL.SDR CALA2017120104241Socket · brokenELECTRICAL ODOR WAS REPORTED BY THE FA''S STATIONED IN THE FWD & MID GALLEY''S DURING T/O. THE FA IN THE FWD GALLEY WAS REPORTED SOME OVERHEAD & SIDEWALL LIGHTING FLICKERING 30 SECS AFTER POWER TRANSFER IN THE FWD GALLEY. THE ODOR WAS THE ODOR WAS SMELT AS FASDR CALA2017100103361Switch · dirtyDOOR 2L DOOR SLIDE ARM LIGHT INTERMITTENT REMOVED DEBRIS. CYCLED SELECTOR SEVERAL TIMES. NO DEFECTS NOTEDSDR CALA2017081402697Lamp · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-06. OPS CHECKED GOOD.SDR CALA2017080802533Lamp · inoperativeFA REPORTED THE R2 DOOR SLIDE LIGHT IS NOT ILLUMINATED AMBER WITH DOOR ARMED. NORMAL PRIOR. FOUND BOTH SLIDE ARMED BULBS INOPERATIVE. REPLACED THE LAMPS, OPERATED ARM LEVER SEVERAL TIMES, SLIDE LAMP OPERATES NORMAL,SDR CALA2017072102323Sensor · dirtyDOOR 2L SLIDE LIGHT INTERMITTENTLY CAME ON NOW WONT ILLUMINATE WITH DOOR ARMED FOUND GIRT BAR RETAINER AND SENSOR DIRTY. CLEANED SENSOR AND REMOVED DEBRIS FROM RETAINER AREA. SLIDE LIGHT NOW CHECKS OK.SDR CALA2017072102285Sensor · out of adjustR2 DOOR SLIDE WILL NOT ARM. FOUND THE GIRT BAR PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED THE SENSOR IAW AMM 25-66-11. OPS CHECKED NORMAL.SDR CALA2017070702105Stiffener · crackedLT AFT WING TO BODY FAIRING 195EL UPPER SUPPORT STIFFENER HAS A CRACK, LOWER END. REMOVED AND REPLACED WITH 1 EA NEW-7 STIFFENER AT LEFT AFT WING TO BODY UPPER SUPPORT IAW SRM 51-40-02 PAR 6.SDR CALA2017070702097Intercostal · crackedAFT CARGO CEILING BS1180+80 TO 1180+100 BL0 HAS CRACKED INTERCOSTAL ANGLE AT FLOOR BOARD NUTPLATES. REMOVED CRACKED UPPER ATTACH ANGLE, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL UPPER ATTACH ANGLE BL0 FS1180+80 TO 1180+100 IAW SRM 51-40-02 PAR 4 AND 51-40SDR CALA2017070702096Attach Angle · crackedMAIN CABIN FLOOR SUPPORT STRUCTURE INTERCOSTAL UPPER ATTACH ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1320 TO BS 1340 BL 0 (VIEW FROM AFT CARGO CEILING). REMOVED CRACKED UPPER ATTACH ANGLE, LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL UPPER ATTACH ANGSDR CALA2017062301931Bracket · damagedNR 2 UPPER PYLON UNDER WING L/E OTBD SIDE HAS CONTROL CABLE RUBBING ON GROMMET AND BRACKET. REMOVED AND REPLACED THE BRACKET AND GROMMET IAW AMM 76-11-03, 20-10-06, SRM 51-4 0-02, AND 51-30-01, CLEARANCE CHECKED GOOD. NO DEFECT NOTED.SDR CALA2017062301930Angle · crackedAFT CARGO CEILING, BS 1180+20 TO 1180+40, BL 0 HAS A CRACKED FLOOR SUPPORT ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, PAR 4, AND 51-40-05, FIG 2.SDR CALA2017061901888Floor Support · crackedMAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1580 TO 1600, BL 0. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4.SDR CALA2017061601834Floor Support · crackedMAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1200 - 1220. MAJOR REPAIR. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-40-02, PAR 4, FIG 8, AND PAR 7D, FIG 14.SDR CALA2017061601833Floor Support · crackedMAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1500 - 1520, BL 0. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-40-02, PAR 4, AND 51-40-05, FIG 2.SDR CALA2017061601832Floor Support · crackedMAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1420 - 1440, BL 0. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-40-02, PAR 4, AND 51-40-05, FIG 2.SDR CALA2017061601831Floor Support · crackedMAIN CABIN FLOOR SUPPORT UPPER ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1260 - 1280, BL 0, REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IAW SRM 51-40-02, PAR 4, AND 51-40-05, FIG 2.SDR CALA2017060501707Lamp · inoperativeEXT EMERGENCY LIGHT INOPERATIVE AT DOOR 2 RIGHT. REPLACED THE LAMPS IAW AMM 33-51-06SDR CALA2017032400710Lamp · inoperativeR1 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06-962-001-002. OPS TESTED GOOD.SDR CALA2017030500539Unknown · odorAFT TO DURING CLIMB OUT FA AT MID AND AFT REPORTED SMELL. COCKPIT ALSO SMELL LIKE HOT PACK. ACCOMPLISHED INSPECTION PER AMM 05-51-58. NO ABNORMALITIES FOUND.SDR CALA2015081100656Light · not seatedEMERGENCY EXIT LIGHT INOPERATIVE IN BULLNOSE AT ROW 5FE. RESEAT LAMP AT ROW 5FE BULLNOSE. EMER LIGHT OPERATIONS CHECKED NORMAL IAW MM 33-51-05.SDR CALA2014062700814Structure · gougedFOUND ON OPEN UP LT HORIZONTAL STAB LE STATION 96, LE GOUGED. ACCOMPLISHED REPAIR IAW ECRA 5510-02437. SEE WORK PERFORMED ON SUB TASKS & WIPS. INITIATE DIP ACCOMPLISHES PERMANENT REPAIR ON OR BEFORE 06/24/2016. PLANNING TO CONTACT ENGINEERING AFTER 04/24/2SDR CALA2014062000761Skin · corrodedFORWARD CARGO BILGE AREA OF FUSELAGE SKIN HAS EXFOLIATION CORROSION ON CHEM MILL AREA, 7 INCHES FWD OF STATION 900 NEXT TO BILGE DRAIN AT BL 0 0. REMOVED CORROSION & INSTALLED DOUBLER & TRIPLER IAW ECRA 5330-04860. DIP WAS INITIATED TO ACCOMPLISH A PERMANENTSDR CALA2014060900731Seat Track · corrodedSEAT TRACK CORRODED BS 1340. REPAIRED SEAT TRACK FROM BS 1320 TO 1450 IAW SRM 53-00-52 REPAIR OPTION 1.
Back to N57868