Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA2010080300362Floorbeam · corrodedCABIN - STA 1661 RBL 0 - RBL 16 FLOORBEAM FOUND CORRODED (CTN CP53-251-01I). CABIN FLOORBEAM UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR 3 FIG 201 AT STA 1661 SDR CALA2010080300361Floor Support · corrodedCABIN STA 1640-1681 LT MOST O/B FLOOR SUPPORT FOUND CORRODED. CABIN FLOOR SUPPORT CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-0SDR CALA2010080300360Floor Support · corrodedCABIN STA 1646-1661 LBL 0 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-02 AT STA 164SDR CALA2010080200358Floor Support · corrodedCABIN STA 1661-1681 LBL 0 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED SUPPORT REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AT STA 1661-1681 LBL 0.SDR CALA2010080300359Oven · dirtyLAV SMOKE EICAS COMES ON FOR AFT LAVS WHEN HOT OVENS ARE OPENED. FOUND OVENS AT POSITIONS 411 AND 413 FILTHY AND UNCLEANABLE. OP'ED OVENS TO HOT AND OVENS SMOKE THE DIRT. REMOVED AND REPLACED OVENS AT 411 AND 413. OPS GOOD. ROTABLE PARTS CHANGE WAS INDICASDR CALA2010073000354Hydraulic Line · leakingHYD QTY DECREASED TO 0 DEBRIEFED CREW ENG AND ELEC PUMPS SHUTOFF WITHIN ONE MIN OF LOW PRESS LIGHT. PER MM 29-11-05 NO MAINT ACTION REQ FOR PUMPS OR FILTERS. FOUND LEAK ON LINE FOR LEFT GEAR DOWNLOCK ACTUATOR. REMOVED AND REPLACED BOTH LINES PER MM 32-32-02SDR CALA2010072700348Fan · malfunctionedELECTRICAL WIRE SMELL CAME FROM F/O VENT AREA UNDER EFB FOR 2 MIN AND WENT AWAY DURING DESCENT, SMELL CAME BACK FOR APPOX 2 MIN & WENT AWAY PERFORMED INSP OF FWD E&E COMPARTMENT . REMOVED AND REPLACED RT RECIRC FAN AS A PRECAUTION, RAN ENGINE TO SIMULATE DISCSDR CALA2010070800330Support Fitting · wornLEFT WING NR 3 FLAP TRACK AFT SUPPORT FITTING FOUND ELONGATED HOLES AT FLAP LOWER PANEL AND LOWER CHORD. REPAIRED AS PER EC/RA 5750-04318 AND FORM 44.0008 ITEMS 1 THRU 9. DIP ISSUED TO "ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 6/29/10.SDR CALA2010070700327Seat Track · corrodedM/D STA 1340-1360 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 1 FIG 201 AT STA 1320 TO STA 1410 LBL 45 AND FORM 44.0008SDR CALA2010070700326Seat Track · corrodedCABIN: STA 1140 - STA 1160 RBL 45 SEAT TRACK LIP FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER AMM 20-11-00 AT CABIN STA 1070 TO STSDR CALA2010070700325Seat Track · corrodedM/D STA 1440-1460 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 1 FIG 201 AT STA 1410-1540 LBL 45 AND FORM 44.0008 ATT ITEM 1-15 ACSDR CALA2010070700324Seat Track · corrodedCABIN STA 1180-1200 RBL 45 SEAT TRACK LIP FOUND CORRODED. SEAT TRACK SCRATCH SMOOTHED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE FIG 101 LIMIT & SEAT TRACK REPLACED AS PER SRM 51-10-02 & NEW SEAT TRACK INSTALLED AS PER AMM 20-11-00 AND SRM 51-40-02 AT STA 1180 TO SSDR CALA2010070700323Seat Track · corrodedCABIN STA 1080-1100 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CROWN CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALLED AS PER AMM 20-11-00 AND FORSDR CALA2010070700322Seat Track · corrodedCABIN STA 1160-1180 LBL 24 SEAT TRACK CROWN AND LIP FOUND CORROSION. CABIN SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER AMM 20-11-00 AT STA 1070 TOSDR CALA2010070700321Seat Track · corrodedM/D STA 1540-1560 LBL 45 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK CORROSION REMOVED OUT OF SRM 53-00-52 ALLOWABLE DAMAGED 1 FIG 101 LIMIT AND CORROSION SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AT STA 1540 - STA 1600 LBL 45SDR CALA2010070700320Floor Support · corrodedCABIN RT STA 685 RBL 18 FLOOR SUPPORT UPPER SURFACE FOUND CORROSION. CABIN RT STA 685 RBL 18 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT & CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 & NEW SUPPORSDR CALA2010070700319Floor Support · corrodedCABIN STA 355 BL 0 FLOOR SUPPORT UPPER SURFACE CORROSION. CABIN STA 355 BL 0 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW SUPPORT INSTALLED SDR CALA2010070700318Floor Support · corrodedCABIN STA 329 BL 0 FLOOR SUPPORT UPPER SURFACE CORROSION. CABIN STA 325 BL 0 FLOOR SUPPORT SUPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION SUPPORT REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-0SDR CALA2010070700317Floor Support · corrodedCABIN RT STA 700-715 RBL 18 FLOOR SUPPORT UPPER SURFACE FOUND CORROSION. CABIN STA 700 TO STA 715 RBL 18 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-10-0SDR CALA2010070700316Floor Support · corrodedCABIN RT STA RBL 50 FLOOR SUPPORT UPPER SURFACE FOUND CORROSION 686 TO 700. CABIN STA 686 TO STA 700 RBL 50 FLOOR SUPPORT UPPER SURFACE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORROSION FLOOR SUPPORT REPLACED AS PER SRM 51-1SDR CALA2010062800313Floorbeam · corrodedCABIN STA 1660 BL 0 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN STA 1660 RBL 5 TO LBL 5 FLOORBEAM UPPER SURFACE REPAIRED AS PER SRM 53-00-51 REPAIR 3 FIG 201.SDR CALA2010062800312Floor Support · corrodedCABIN BS 1640 LBL 15 - RBL 6 FLOOR SUPPORT FOUND CORRODED. CABIN BS 1640 LBL 15 - LBL 10 CORROSION REMOVED AS PER SRM 51-10-02 AND RE-PROTECTED AS PER SRM 51-20-01 BLEND AREA LENGTH 1"X WIDTH 1" X DEPTH 0.005" ORIG 0.125" WITHIN SRM 53-00-51 FIG 101. ALLOWABSDR CALA2010062800311Shear Web · corrodedCABIN BS 1680 LBL 52 - RBL 52 FLOOR SHEAR WEB UPPER SURFACE FOUND CORRODED. CABIN BS 1680 LBL 25 - LBL 23 FL SHEAR WEB REPAIRED AS PER SRM 53-60- 51 REPAIR 2 FIG 201. HFEC NIL CRACK FOUND OTHER AREA CORROSION REMOVED AS PER SRM 51-10-02 & RE-PROTECTED AS PERSDR CALA2010062800310Floorbeam · corrodedCABIN LT STA 365.25 BL 0 - RBL 10 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 365.25 BL 0 - RBL10 FLOORBEAM UPPER FLANGE REPLACED AS PER SRM 53-00-51 REPAIR 5 FIG 201.SDR CALA2010062800309Floor Support · corrodedCABIN BS 1660-1680 RBL 60 FLOOR SUPPORT FOUND CORRODED. CABIN BS 1660-1680 RBL 60 FLOOR SUPPORT REPLACED AS PER SRM 51-10-02.SDR CALA2010062800308Floor Support · corrodedCABIN BS 1650-1680 LBL 60 FLOOR SUPPORT FOUND CORRODED. CABIN BS 1650-1660 LBL 60 FLOOR SUPPORT CORROSION REMOVED AS PER SRM51-10-02 & RE-PROTECTED AS PER SRM 51-20-01 BLEND AREA LENGTH 2"X WIDTH 1"X DEPTH 0.005" WITHIN SRM 53-00-51 FIG 101 ALLOWABLE DAMAGE LSDR CALA2010062200295Collar · crackedR4 DOOR DIFFICULT TO OPEN. DOOR 4R GUST LOCK COLLAR CRACKED REMOVED AND REPLACED GUST LOCK COLLAR ON DOOR 4R IAW AMM 52-11-08-358-001. DOOR OPS NORMAL. P/N 140N6008-16 B/N 198716. COLLAR ASSY PERFORMED IDT.SDR CALA2010061000261Failsafe · corrodedAFT CARGO COMPARTMENT-BELT FRAME EXFOLIATED ABOVE S 29L AT STA 1480. REPAIRED BS 1480 LOWER FRAME FAIL SAFE CORD REF ECRA 5311-01492. INTERIM REPAIR ACCOMPLISHED PER ECRA 5311-01492, PART 1. ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 06/07/2010. PSDR CALA2010061000265Beltframe · corrodedAFT CARGO COMPARTMENT - BELT FRAME EXFOLIATED ABOVE STR 26 RT STA 1520. REPAIRED BELT FRAME REF SRM 53-00-07 REPAIR 5. ISSUED DIP FOR REP INSPECTION REF 53-00-07 REPAIR 5 FIG 201 TABLE 2 ZONE 1 REQUIREMENTS. REINSPECT BELT FRAME REPAIR STA 1520 ABOVE STRINGSDR CALA2010061000264Skin · puncturedSUPPORT TASK: R4 DOOR INTERIOR SKIN HAS SMALL PUNCTURE LOCATED A T UPPER HINGE ARM ASSY. REPAIRED R4 DOOR INNER SKIN AT HINGE CUTOUT REF ECRA 5210-02155 ISSUED DIP FOR PERMANENT REPAIR WITHIN 24 MONTHS. INTERIM REPAIR ACCOMPLISHED PER ECRA 5210-02155, PART SDR CALA2010061000263Skin · misrepairedEXTERIOR FUSELAGE SKIN STA 630& S28L. EXISTING REPAIR FASTENERS EDGE DISTANCE ED NOT PER SRM. ACCOMPLISHED FUSELAGE SKIN INTERIM REPAIR STA 590-630 S13L TO S 18L REF ECRA 5330-04028. ISSUED DIP INTERIM REPAIR ACCOMPLISHED PER ECRA 5330-04028, PART 1. ACCOSDR CALA2010061000262Skin · dentedEXTERIOR FUSELAGE SKIN HAS DENT AT STA 754 S17L. REPAIRED EXTERIOR FUSELAGE SKIN STA 750-777 S14L TO S18L. REF ECRA 5330-04027. INTERIM REPAIR ACCOMPLISHED PER ECRA 5330-04027, PART 1. ACCOMPLISH A PERMANENT REPAIR BEFORE 37,500 TOTAL FLIGHT CYCLES. PLANNSDR CALA2010061000260Sill · damagedSUPPORT TASK: L2 DOOR CUTOUT AT UPPER SILL, OUTER CORD HAS ACCIDENTAL DRILL DAMAGE AT STA 720. REPAIRED UPPER SILL STRAP REF ECRA 5310-05187 ISSUED DIP FOR PERMANENT REPAIR WITHIN 24 MONTHS. INTERIM REPAIR ACCOMPLISHED PER ECRA 5310-05187, PART 1. ACCOMPLISDR CALA2010060900259Static Line · leakingAFTER TAKEOFF ENCOUNTERED NUMEROUS EICAS MESSAGES L+R ENG EEC, IAS DISAGREE, ALT DISAGREE + AUTO SPD BRAKE. AFTER SELECTING F/O AIRDATA TO ALTN, EICAS MESSAGE WENT AWAY. REMOVED AND REPLACED LEAKING RIGHT STATIC LINE 19-3411-3-0021 REF IPC 34-11-51-10A ITEM SDR CALA2010060800249Stringer · corrodedAFT CARGO COMPARTMENT - STRINGER EXFOLIATED AT BS 1472 BL 0. CUT OUT DAMAGED STRINGER SECTION, DRILLED UP NEW SECTION AND REPAIR SPLICE AND INSTALLED ALL REPAIR PARTS. REF SRM 53-60-0 3 AND 53-00-03 REPAIR 1.SDR CALA2010060300247Stringer · corrodedGENERATED DIP FOR N/R 9914225 FOR AFT CARGO COMPARTMENT STRINGER REF SRM 53-00-03 REPAIR 1. EXFOLIATED AT BS 1472 BL 0. 53-DIP CONTROL 05390. INSPECTION THRESHOLD IS 37,500 WITH REPEAT INSPECTIONS OF 3,000 FLIGHT CYCLES. PERFORM INITIAL INSPECTION OF REPAIRSDR CALA2010060200243Shutoff Valve · failedHIGH STAGE BLEED LIGHT FIRST AND ENGINE OVERHEAT LIGHT ON LT ENGINE. PERFORMED FIM TASK 36-10-00. HIGH STAGE LIGHT ILLUM. R & AMP; R HIGH STAGE PILOT AND HPSOV. RAN ENGINE AT TAKEOFF POWER NO BLEED LIGHT OR OVERHEAT LIGHT CAME ON. ROTABLE PARTS CHANGE WAS INDISDR CALA2010052700226Beltframe · crackedCABIN BELTFRAME CRACKED AT LT SIDE STA 1580 BETWEEN STRINGERS 8LT AND 9LT INSTALLED REPAIR AT STA 1580 LT SIDE BETWEEN STRINGER 8LT AND 9LT. ISSUED DIP 05262 TO PERFORM DETAILED VISUAL INSP AT 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COSDR CALA2010052700225Beltframe · crackedCABIN BELTFRAME CRACKED AT RT SIDE STA 1580 BETWEEN STRINGERS 8RT AND 9RT. INSTALLED REPAIR AT STA 1580 RT SIDE BETWEEN STRINGER 8RT AND 9RT. ISSUED DIP TO PERFORM DETAILED VISUAL INSP AT 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES SDR CALA2010052700224Beltframe · crackedCABIN BELTFRAME CRACKED AT STA 760 RT SIDE BETWEEN STRINGERS 8RT AND 9RT. INSTALLED REPAIR AT STA 760 BELTFRAME STRINGER BETWEEN 8RT AND 9RT REF SRM 53-00-07 REPAIR 1.SDR CALA2010052700221Track · dirtyDOOR 1L IS HARD TO ARM AND LIGHT DOES NOT COME ON. CLEANED TRACK ON DOOR 1L, INSTALLED COVER, OPS CHECKS GOOD. OK TO CONTINUE, LIGHT COME ON WHEN ARMED. AMM REF 52-11-00-603.SDR CALA2010052000219Oven · overheatedFIRST CLASS OVEN 205 OVERHEATED AND THE COILS WERE BRIGHT RED. THERE WAS AN ELECTRICAL SMELL AND THE FLIGHT ATTENDANT TURNED THE OVEN OFF AND PULLED IT'S CIRCUIT BREAKER. ACCOMPLISHED AM PROCEDURE 05-51-58. OVEN DEFERRED. REPLACED OVEN NR 205. CHECKS OK. SDR CALA2010052000218Oven · malfunctionedAFT GALLEY OVEN 413 SMOKES EXCESSIVELY AND SETS OFF LAV SMOKE DETECTOR. PLACED AFT GALLEY OVEN POS 413 ON MEL. OK TO CONT. PULLED AND COLLARD C/B. REMOVED AND REPLACED NR 413 AFT OVEN. ALL FUNCTIONS NORMAL AT THIS TIME. PLACARD REMOVED. ROTABLE PARTS CHSDR CALA2010052000215Door · damagedWHILE AIRCRAFT PARKED, PUSHBACK TRACTOR PUSHED A/C AFT APPROX 5 TO 8 FEET, REFER TO LP 8424115, 8424116 AND 8424118 FOR DISCREPANCIES. L/P 8424115, 8424116 & 8424118 HAS BEEN C/W. L-1 DOOR WAS REMOVED, SHIPPED TO HOBBY SHOP FOR REPAIR, THEN SHIPPED BACK TO ESDR CALA2010052000213Oven · activatedFIRST CLASS OVEN NR 205 SMOKE AND SMELL OF BURNING. PLACED THE ABOVE ITEM ON PLACARD NR 25-P-31F. CONTROL NUMBER 510507. C/B PULLED AND COLLARED.SDR CALA2010051100195Crease Beam · corrodedSUPPORT TASK. CABIN FLOOR STRUCTURE, O/B CREASE BEAM CHORD AT STA 1040 RBL 65 HAS LIGHT SURFACE CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLES AND SHIMS REF ECRA 5310-05170. CREATED DIP WITH THIS LOG PAGE ITEM 53-DIP CONTROL NUMBER 050SDR CALA2010042600160Oven · defectiveBURNING SMELL, SMOKE FROM NR 205 FWD GALLEY. PULLED CIRCUIT BREAKER. PLACARD OVEN NR 205 INOP. BREAKER PULLED AND COLLARED. NEEDS OVEN 99-2532-9-0003. NO TIME DUE TO QUICK TURN INBOARD DISCREPANCIES. EXT 084979.SDR CALA2010042600157Flap · malfunctionedT/E FLAP DISAGREE LT ON APPROACH PERFORMED FIM TASK 27-51-00 FIG 104, NO FAULTS FOUND ALL INDICATIONS NORMAL. PERFORMED AMM 27-58-00 501, OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.SDR CALA2010041400137Stiffener · wornSUPPORT TASK, RT WING FRONT SPAR WEB STIFFENER IS WORN INTO BY BLEED AIR DUCT SUPPORT CLAMP FSS 148.9. REMOVED AND REPLACED RT WING FRONT SPAR STIFFENER AT FSS 148.9 REF ECRA 5710-02179.SDR CALA2010041200129Beltframe · wornCABIN INTERIOR, BELT FRAME AT STA 1681 S11R HAS WEAR MARK FROM SIDEWALL PANEL ATTACH BRACKET. BLENDED OUT DAMAGE, INSTALLED A REPAIR DOUBLER AND INITIATED A DIP (53-DIP CONTROL NUMBER 004497) TO ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM APRIL 07 - 2
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