Boeing 757-225
Service difficulty reports · 1,988
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '757225' 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 aircraft_model_key = '757225' 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 USAA010926Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH AREA, BS 440, LBL 45. CORROSION LEVEL 1, TASK NR C53-231-02. DAMAGE REMOVED, SPLICED IN REPAIR SECTION PER SRM 53-00-52. (M)SDR USAA010920Web · crackedCLT - FOUND CREASE BEAM WEB CRACKED APPROXIMATELY .25 INCH, JUST FORWARD OF BS 1380, RBL 64. INSTALLED REPAIR DOUBLER AND CREASE BEAM ANGLE PER SRM 51-70-13. (M)SDR USAA010915Doubler · corrodedCLT - FOUND A 2 INCH AREA OF FRAME CORRODED, BS 640, MID CHORD, BETWEEN S25R AND S26R. CORROSION REMOVED, INSTALLED REPAIR DOUBLER PER SRM 51-10-02. (M)SDR USAA010913Frame · gougedCLT - FOUND FRAME GOUGED APPROXIMATELY .25 INCH, BS 1340 AT S26L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-01. (M)SDR USAA010912Stringer · crackedCLT - FOUND STRINGER CRACKED, BS 466, STRINGER 21R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-00-03. (M)SDR USAA010919Doubler · crackedCLT - FOUND PYLON INT DOUBLER CRACKED .5 INCH, NR 1 PYLON PP STATION 107, LOWER FORWARD CORNER, PANEL NR 433AL. INSTALLED REPAIR DOUBLER PLATE PER EA 85055. (M)SDR USAA010918Frame · dentedCLT - FOUND FRAME DENTED APPROXIMATELY .5 INCH, BS 700 AT S23L. INSTALLED REPAIR DOUBLER PER EA 85014. (M)SDR USAA010914Frame · dentedCLT - FOUND FRAME DENTED APPROXIMATELY .25 INCH IN DIAMETER, BS 620 AT S24L. INSTALLED REPAIR DOUBLER PER EA 69875. (M)SDR USAA010917Frame · dentedCLT - FOUND FRAME DENTED APPROX .25 INCH IN DIAMETER, BS 600 BETWEEN S23L AND S24L. INSTALLED REPAIR DOUBLER PER EA 69874. (M)SDR USAA010916Frame · dentedCLT - FOUND FRAME DENTED APPROX .25 INCH IN DIAMETER, BS 580 ABOVE S23L. INSTALLED REPAIR DUOBLER PER EA 69872. (M)SDR USAA010930Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH AREA, BS 660, RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-00-52. (M)SDR USAA010935SkinCLT - FOUND LIGHTNING STRIKE ON FUSELAGE SKIN, BS 373 BETWEEN S25R AND S26R. PREVIOUSLY INSTALLED .21875 RIVET PER SRM 53-00-01, FIG 207. (M)SDR AWXA0002049Skin · damagedFS 395 STR 21-L EXTERNAL DOUBLER NOT PER SRM. REMOVED EXISTING REPAIR DOUBLER. FABRICATED AND INSTALLED REPAIR DOUBLER PER AWA ER 19-5331-01198-SS1.SDR AWXA0002043Hydraulic Line · leakingLAS- UNSCHEDULED LANDING- FLT 46 - AFTER DEPARTURE FROM FLL EN ROUTE TO LAS THE AIRCRAFT LOST LEFT HYDRAULIC SYSTEM QUANTITY AND DIVERTED TO MCO. THE AIRCRAFT MADE AN UNEVENTFUL, OVER WEIGHT LANDING (231,000LBS). IN MCO MAINTENANCE TROUBLESHOT AND FOUND A RTSDR USAABB01071Charger · inoperativeBDL - FOUND EMERGENCY LIGHTS AT ROWS 9, 10, 12, 14, 18 AND THE L2 DOOR INOPERATIVE. MAINTENANCE REPLACED THE M733 BATTERY CHARGER AND PACK. (M)SDR AWXA0002005Stringer · crackedd: Stringer 24L at STA 525C: Removed damaged area on stringer, Fabricated and installed repair per SRM 53-00-03 fig 201SDR USAA010911Frame · dentedCLT - FOUND FRAME DENTED .5 INCH IN DIAMETER, BS 1600, BETWEEN S25R AND S26R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EA 69860. (M)SDR AWXA0002038Intercostal · corrodedD: Pas. Cabin RBL 54 STA 377-420 Intercostal corroded top surface around fastner holes.C: Removed intercostal, Fabbed & Installed Intercostal per SRM 51-40-02 pg 46-47 Fig 12 & SRM 57-30-01 pg 11 step 7SDR AWXA0002046Flap · chafedLEFT O/B FORE FLAP LEADING EDGE I/B AREA WS 397-438 HAS SEVERAL CHAFED MARKS. BLENDED OUT CHAFED AREAS, ORIG MAT .080-MAT LOSS .020, OUT OF LIMITS, CUT OUT DAMAGE. FABBED REPAIR PLATE DOUBLERS AND STRAPS IAW SRM 57-33-01. INSTALLED PARTS IAW SRM 57-53-01 FISDR AWXA0002037Intercostal · crackedD: Intercostal cracked at STA 446 between STR 22L & 23LC: Removed cracked intercostal at STA 446-460, 23L. Installed replacement intercoastal at STA 440-460, 23L IAW SRM 51-40-02 Pg 4SDR AWXA0002065Angle · crackedD: Aft cargo compartment BS 1661 RBL intercostal topflange cracked.C: replaced angle IAW SRM 53-60-51SDR AWXA0002001Support · corrodedPASSENGER CABIN SEAT TRACK B/S 400 RBL 26 TO B/S 420 CORRODED. REMOVED CROWN SEAT TRACK STA 400 TO STA 420, REMOVED SUPPORT BEAM, INSTALLED NEW SUPPORT BEAM, REINSTALLED SEAT TRACK, CHANNELS AND INTERCOSTAL PER SRM 51-40-02 PAGE 11 & 12.SDR AWXA0001992Seat Track · corrodedPASSENGER CABIN SEAT TRACK TOP FLANGE CORRODED AROUND FASTENER HOLES B/S 420, RBL 44. REMOVED AND REPLACED SEAT TRACK SUPPORT B/S 420, RBL 44, IAW SRM 51-40-02 FIG 12 PAGE 42.SDR AWXA0002042Seat Track · corrodedD: Pass. Cabin BS 395-377 seat track corroded @ RBL 24 O/B flangeC: Removed damaged channel (track) IAW SRM 51-40-05 fig 39-40. Fabricated track, treated primed, installed per SRM 51-40-02 pg 26 SRM 51-20-01 pg 1-3 SRM 51-30-01 pg 11 (STA 395-377,RBL 24) and pSDR AWXA0002003Floorbeam · corrodedPASSENGER CABIN FLOORBEAM BS 377, BL 0 TO LBL 24, UPPER T-CAP TOP FLANGE AND LOWER SURFACE CORRODED. CUT OUT DAMAGED SECTION OF UPPER T-CAP FLOORBEAM. FABRICATED NEW SECTION OF BEAM AND REPAIR SPLICE ANGLES AND INSTALLED ALL THE NEW REPAIR PARTS AND PREVIOUSSDR USAABB01063Light · inoperativeBWI - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)SDR USAABB01062Battery · dischargedBWI - FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 6 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M)SDR AWXA0001965Servo · malfunctionedEN ROUTE FROM PHX TO MCO AT FL 370 THE AIRCRAFT MADE A SUDDEN ROLL OF 20-30 DEGREES TO THE LEFT. AUTO PILOT DISENGAGED. AFTER RECOVERY TO LEVEL OF FLIGHT, NO ADVERSE YAW OR OUT OF TRIM COND EVIDENT. JUST PRIOR TO ROLL, EPR'S MATCHED, BUT N1, N2, N3, EGT & FSDR USAA010767Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 2 INCH AREA, BS 1320 RBL 62. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-51, FIG 205. (M)SDR USAA010773SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 8.5 INCHES BY 11.5 INCHES, BS 1620, BETWEEN S17L AND S19L. DOUBLER INSTALLED PER EA 66107-A, SRM 53-60-01 FIG 101 AND 53-00-01 FIG 204. (M)SDR USAA010772SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 2.5 INCHES BY 3 INCHES, BS 423, BETWEEN S16L AND S17L. DOUBLER INSTALLED PER SRM 53-00-01, FIG 206. (M)SDR USAA010771Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED IN TWO PLACES .5 INCH EACH, BS 1620, S18R. REMOVED AND REPLACED TIE CLIP PER SRM 51-40-00. (M)SDR USAA010770Channel · crackedCLT - FOUND CHANNEL CRACKED .75 INCH, BS 310.5, LBL 20, FORWARD SIDE OF FLOORBEAM. REMOVED AND REPLACED PER SRM 51-40-02. (M)SDR USAA010769SkinCLT - FOUND SKIN PREVIOUSLY INSTALLED DOUBLER, BS 902, S3R. DOUBLER INSTALLED PER SRM 53-00-01, FIG 203. (M)SDR USAA010768Frame · dentedCLT - FOUND FRAME DENTED .5 INCH DIAMETER, BS 1540, OUTBOARD OF S26L. DAMAGE REMOVED, FABRICATED AND INSTALLED DOUBLER AND STRINGER TIE CLIPS PER TR 53-60-01, AND EA 69860. (M)SDR AWXA0001913Skin · puncturedD: 1.5" x 1.5" hole in fuselage below & fwd of L-4 door below STR 21LC: repaired per E.R. 19-5331-01171-DL3SDR AWXA0001912Skin · dentedD: Fuselage skin STA 640 between STR 17L and 15L is dented and has 3 existing doublers which do not meet SRM seperation requirements.C: Repaired damaged skin per E.R. 19-5331-01179- DOISDR AWXA0001911Stringer · dentedD: Found Stringer 16L at Sta 623 to have dent C: Removed damaged stringer section and installed repair IAW SRM 530-00-03 Fig 201SDR AWXA0001910Skin · dentedDENT IN AIRCRAFT SKIN AFT OF L-4 DOOR STA 1720 BETWEEN STRINGERS 13L & 14L. CUT OUT DAMAGE 1.5 X 2.2 AREA OF SKIN, FABBED AND INSTALLED INTERNAL DOUBLER PER 53-00-01, NDT NO CRACKS NOTED PER NTM 51-00-19.SDR USAABB01045Battery · dischargedLAX - FOUND LOW LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 1, 4, 22, 29 AND 33. MAINTENANCE REPLACED THE BATTERIES. (M)SDR USAABB01041Light · inoperativeMCO - MAINTENANCE FOUND THE EMERGENCY LIGHT MOUNTED AT SEAT 33 WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAA010646Channel · corrodedCLT - FOUND U-CHANNEL CORRODED 20 INCHES BY 2 INCH AREA, BS 560-580, BETWEEN STRINGERS 27R AND 28R. FABRICATED AND INSTALLED NEW U-CHANNEL PER SRM 53-30-04 AND 51-10-02. (M)SDR USAA010645Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED .5 INCH BY 1 INCH AREA, BS 690, BELLY, LEFT FORWARD ANTENNA MOUNT. DAMAGE REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLERS PER EA 69727. (M)SDR USAA010620Skin · corrodedCLT - FOUND FUSELAGE INNER SKIN CORRODED APPROXIMATELY 2 SQUARE INCHES, BS 584, STRINGER 28R. REMOVED DAMAGE, INSTALLED DOUBLER AND TRIPLER PER EA 69643. (M)SDR USAA010610Stringer · corrodedCLT - FOUND STRINGER CORRODED APPROXIMATELY 8 SQUARE INCH AREA, BS 555 TO 600, STRINGER 28R. DAMAGE REMOVED, INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-03. (M)SDR USAA010606Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED APPROXIMATELY 6 SQUARE INCH AREA NUT PLATE HOLES, BS 345, RBL 12 TO RBL 52. REMOVED DAMAGED AREA, INSTALLED NEW T-CAP PER TYPICAL REPAIR 53-15-01. (M)SDR USAA010607Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH AREA, BS 360, RBL 13. REMOVED DAMAGE, INSTALLED DOUBLER PER RM 53-10-51. (M)SDR USAA010604Stringer · corrodedCLT - FOUND STRINGER CORRODED 4 INCH AREA, BS 600 TO 660, STRINGER 28L. REMOVED DAMAGE, INSTALLED STRINGER SPLICE REPAIR PER SRM 53-00-03, FIG 201. (M)SDR USAA010612Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED, APPROXIMATELY 2 INCH BY 6 INCH AREA, BS 324, LBL 23 TO LBL 41. DAMAGE REMOVED, REPAIR STRAP AND SLEEVE INSTALLED PER SRM 53-10-08 FIG 101, 51-20-07, AND EA 69647. (M)SDR USAA010609Shear Tie · corrodedCLT - FOUND SHEAR TIE CORRODED 1 INCH BY 4 INCH AREA, BS 1701, BETWEEN S28L AND S28R. REMOVED AND REPLACED SHEAR TIE CLIPS PER SRM 51-20-01 AND EA 69735. (M)
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