Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA201503180955Floorbeam · chafedBS 1540, LBL 10 - RBL 14.75 FLOORBEAM UPPER FLANGE UPPER SURFACE FOUND CHAFED. REPAIRED IAW EA F-5310-T0318496. CLASSIFIED AS MAJOR.SDR FDEA201503160945Skin · gougedLOWER FUSELAGE SKIN, STATION 507 - 508, STRINGER 27 - 28R, HAS GOUGE. ACCOMPLISHED IAW EA F-5330-T0315849 PT 1. CAT B REPAIR IAW FORM 8100-9 DATED 12 MAR 2015. 1ST & 2ND STAGE APPROVAL. DTA PENDING DUE PRIOR TO 60,100 FLIGHT CYCLES.SDR CALA2015031793436Slider · defectiveDOOR 4R SLIDE ARMED LIGHT INOPERATIVE. REPLACED FWD GIRT BAR SLIDER IAW 52-11-25.SDR FDEA201503130910None · noneL1 DOOR WILL NOT ARM. OPERATED & ARMED L1 DOOR EMERGENCY SLIDE IAW AMM 52-11-00-6. OPS CHECKED GOOD.SDR FDEA201503130913Torque Tube · corrodedLEFT INBD FLAP TORQUE TUBE INTERNAL CAVITY CORRODED. REMOVED LOWER INBD STRESS PANEL IAW SRM 51-40-02. R & R INBD FLAP, INBD TORQUE TUBE IAW CMM 57-53-43. REINSTALLED LOWER INBD STRESS PANEL IAW SRM 51-40-02. CORROSION FOUND OUT OF LIMITS IAW CMM 57-53-43 SDR FDEA201503120858Skin · delaminatedRIGHT INBD AFT FLAP OTBD UPPER CORNER SKIN HAS DELAMINATION. REPAIRED IAW 51-70-04 PARA 4. MAJOR REPAIR.SDR FDEA201503120857Skin · dentedRIGHT INBD FLAP, LOWER SURFACE TE WEDGE HAS THREE DENTS, OTBD OF AFT FLAP 5.5" FROM TE. REPAIRED IAW 51-70-10 REPAIR 4. MAJOR REPAIR.SDR FDEA201503120860Crease Beam · corrodedBS 960 - 984 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 114. CREASE BEAM WEB, SHEAR WEB, REMOVED IAW SRM 51-40-02 REV 114. FABRICATED & INSTALLED IAW DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503120859Crease Beam · corrodedBS 920 - 940 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 114. REMOVED CREASE BEAM WEB, SHEAR WEB IAW SRM 51-40-02 REV 114. FABRICATED & INSTALLED IAW DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.SDR CALA2015031793428Doubler · damagedDOOR 4L HAS DAMAGE TO THE INTERNAL SKIN DOUBLER REPAIR. REMOVED, FABRICATED & INSTALLED NEW REPAIR DOUBLER ON R4 DOOR INNER STRUCTURE IAW ECRA 5210-02405 STEPS 5, 13 & 20 - 31.SDR FDEA201503110814Crease Beam · corrodedCABIN STATION 1061 RT CREASE BEAM WEB FOUND CORROSION. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 01 REV & INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110813Crease Beam · corrodedBS 1120 - 1140 LT CREASE BEAM WEB FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 01 REV & INSTALLED IAW DWG 144N5200 SHT 2 REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110812Crease Beam · corrodedBS 1080 - 1100 LT CREASE BEAM WEB FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 01 REV & INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110809Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110808Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110807Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1520 - 1540 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110806Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110805Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1560 - 1580 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110804Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1560 - 1580 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110803Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1580 - 1600 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110802Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1580 - 1600 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110801Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1580 - 1600 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110800Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110799Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110798Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110797Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503110796Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1560 - 1580 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T60316044 PART 1.SDR FDEA201503110795Skin · damagedFUSELAGE, EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503100787Stringer Splice · corrodedAFT CARGO COMPARTMENT AT STATION 1460, STRINGER 23L, SPLICE IS CORRODED.SDR FDEA201503070718Stringer Splice · corrodedAFT CARGO COMPARTMENT AT BS 1460, STRINGER SPLICE 21L CORRODED.SDR FDEA201503060705Skin · damagedVERTICAL STAB SKIN LT SIDE ONE EACH BUTTON HEAD FASTENER INSTALLED. BETWEEN BS 1790 & FSS 245.6. REPAIRED VERTICAL STAB SKIN LH FWD SIDE IAW SRM 51-70-10, PARAGRAPH 19, BS 1790, FSS 245.6. MAJOR REPAIR.SDR FDEA201503060697Pan · corrodedFORWARD CARGO COMPARTMENT STATION 700 - 720, STRINGER 20L - 22L MIDDLE WASTE SERVICE PAN UPPER DOUBLER PLATE CORRODED. REMOVED PER SRM 51-10-02 REV 113 AND FOUND OUT OF LIMITS IAW SRM 53-00-53 FIG 101 ALLOWABLE DAMAGE 1 REV 114 PART 1 OF EA F-5310-T0315975.SDR FDEA201503060703Skin · dentedAFT LOWER FUSELAGE, TWO EACH DENTS WITH SCRATCHES AT STATION 1394, BETWEEN STRINGER 27R - 28R. ACCOMPLISHED EA F-5330-T0315686, P T 1.SDR FDEA201503040656Seat Track · corrodedMAIN DECK COMPARTMENT, STATION 640 - 700, RBL 24.75, SEAT TRACK HAS NICKS, SCRATCHES & CORROSION. R & R SEAT TRACK SUPPORT CROWN IAW SRM 51-40-02 & DWG 143N5080. NOTED DAMAGES ON OLD PART WERE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAILS VII & VIII. MAJORSDR FDEA201503020626Skin · damagedTWO ELONGATED HOLES FOUND ON THE EXTERIOR SKIN AT BS 1360, STRINGER 21 - 22L AFTER DOUBLER REMOVED. REPAIRED IAW EA F-5330-T0315211A PART 1. REPAIR CLASSIFIED AS MAJORSDR CALA2015030493199Floorbeam · corrodedFORWARD FUSELAGE STATION 324, RBL 59 HAS CORROSION AT FASTENER HOLES. BLENDED THE CORROSION & DETERMINED IT TO BE OUT OF LIMITS IAW SRM 51-10-02. EA 130893 & ECRA 5310-05820 WERE ISSUED TO ADDRESS THE DAMAGE. IAW ECRA 5310-05820 REV A, INSPECTION OF THE BS SDR CALA2015030493198Frame · corrodedAFT PIT BS 1480 FRAME CORRODED BETWEEN STRINGER 26 & 27 RT. REMOVED CORROSION IAW STM 51-10-02 & FOUND IT TO BE OUT OF LIMITS IAW SRM 53-02-07 & SRM 53-30-07. EA 130911 & ECRA 5360-01340 WERE ISSUED TO ADDRESS THE DAMAGE. IAW ECRA 5360-01340, THE BS 1480 BESDR CALA2015030493197Skin · dentedFUSELAGE DENT 5 FT FWD OF DOOR 2L AT FLOOR LINE. MEASURES .75" X .062" DEEP. DENT IS CRACK FREE & MUST BE REPAIRED BY NEXT C CHECK. THE DENT WAS FOUND OUT OF LIMITS IAW SRM 53-00-03. THE REPAIR AT BS 605 - 618 FUSELAGE BETWEEN STRINGER 15L & 18L HAS BEEN ASDR CALA2015030493195Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED AT BS 324 BETWEEN RBL 40R - 64R. REMOVED DAMAGED SECTION OF T CAP. FABRICATED & INSTALLED T CAP SPLICE REPAIR ANGLES & STRAPS IAW REO G16382 REV A & SRM 53-10-08 REPAIR 1 IAW ECRA 5310-05795 THIS IS A CAT B REPAIR. THE THRESHOLSDR CALA2015030493194Frame · bentAFT CARGO FRAME BENT STATION 1400, STRINGER 26L TO 27L. REPAIR DAMAGE FRAME IAW SRM 53-00-07 REPAIR 5 DETAIL I. THIS REPAIR IS A CAT B REPAIR IN ZONE 3. REQUIRES SUPPLEMENTAL INSPECTIONS STARTING IN 12,000 FLIGHT CYCLES & 11,000 FLIGHT CYCLES THEREAFTER THISDR CALA2015030493193Frame · dentedAFT CARGO FRAME DENTED STATION 1540, STRINGER 26L. CUT OUT DAMAGED SECTION OF INBD FLANGE & FORMED REPAIR ANGLE IAW SRM 53-00-07 REPAIR 5. INSTALLED IAW SRM 53-00-07 REPAIR 5 TABLE II. THIS IS A CAT B REPAIR IN ZONE 1 & REQUIRES SUPPLEMENTAL INSPECTIONS BEGSDR CALA2015030493192Frame · dentedAIRCRAFT CARGO FRAME DENTED STATION 1420, STRINGER 27L. CUT OUT DAMAGED AREA OF FRAME INBD FLANGE & FORMED A REPAIR ANGLE IAW SRM 53-00-07 REPAIR 5 & INSTALLED. THIS IS A CAT B REPAIR IN ZONE 3 & REQUIRES SUPPLEMENTAL INSPECTIONS TO BEGIN 12,000 CYCLES AFTERSDR CALA2015030493190Skin · damagedTHIS NON-ROUTINE IS TO CAPTURE FABRICATION OF THE REPAIR DOUBLER AT BS 1393, BL0, IAW COA 50745 & TASK CARD 59745401C, DUE TO THIS REPAIR CAN BE ACCOMPLISHED IAW THE SRM WITHOUT DEVIATION. TRIMMED OUT SKIN & FABRICATED & INSTALLED A REPAIR DOUBLER IAW REO G15SDR CALA2015030493185Skin · corrodedAFT CARGO CIRCUMFERENTIAL STRAP & FUSELAGE SKIN CORRODED BS 1400, STRINGER 27L - 28L. REMOVED PREVIOUSLY INSTALLED DOUBLER & CIRCUMFERENTIAL STRAP SPLICE SECTION. FABRICATED & INSTALLED 6 STRAIGHT SHANK FREEZE PLUGS, REPAIR DOUBLER, 146N3810-8200 SKIN SPLICESDR CALA2015030293183Unknown · malfunctionedLEADING EDGE & TE FLAP DISAGREE AT 20. CREW SELECTED FLAP 30, BUT FLAP WAS STOPPED AT 22, USED ALT TO PUT FLAP AT 20 & DIVERTED. TEST ON FSEU IAW AMM 27-51-01, ALSO DID A VISUAL INSP OF FLAPS, FOUND NO DEFECTS.SDR CALA2015030993400Structure · crackedL2 DOOR UPPER HINGE CUT OUT CRACKED. REMOVE, MFG & INSTALLED PART 1 ANGLE IAW SRM 52-10-02 REPAIR 1.SDR CALA2015030493201Angle · crackedL2 DOOR UPPER HINGE CUT OUT CRACKED. REMOVED, MFG & INSTALLED PART 1 ANGLE IAW SRM 52-10-02 REPAIR 1. CF REQUIRED TO INSPECT IAW B TABLE 202 AT 50000 DOOR FLIGHT CYCLES OR 5800 FLIGHT CYCLES AFTER REPAIR INSTALLED IF THE DOOR FLIGHT CYCLES ARE NOT KNOWN.SDR CALA2015030493189Unknown · smokeSMOKE IN COCKPIT & CABIN AT CLIMB POWER WITH LT PACK RUNNING. TURNING OFF PACK STOPS SMOKE REF SERVICE TIP MM 79-00-95-901. DEFERRED LT PACK IAW MEL 2151A. AIRPLANE SOLD AS IS ON 27 FEB 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.SDR FDEA201502250596Angle · corrodedAPU AIR INTAKE LOWER CUT OUT FLANGE IS EXFOLIATED. L REMOVE CORROSION FROM 2 EA ANGLES AT APE AIR INTAKE DUCT. LOWER CUT OUT YAW SUM 51-10-02. BLENDED TWO EACH ANGLES ORIGINAL MAT , LOSS .06 INCHES , REMAINING .000", FOUND 2EA. ANGLES OUT OF LIMITS AS PESDR FDEA201502250595Duct · corrodedAPU AIR INTAKE DUCT FWD CUT OUT FLANGE IS EXFOLIATED. REMOVED CORROSION FROM FWD CUT OUT FLANGE AT APU AIR INTAKE AS PER SRM 51-10-02. BLEND STRAP ORIG. MAT. .250", MAT. LOSS .250", REMAINING .000", FOUND OUT OF LIMITS AS PER SRM 53-00-01, FIG. 101, DETAI
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