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 CALA2015072700611Skin · gougedDAMAGE WAS A GOUGE AT LEFT FUSELAGE SKIN BELOW LEFT HORIZONTAL STABILIZER. INSTALLED REPAIR PARTS & APPLIED CORROSION INHIBITING COMPOUND TO INSIDE OF REPAIR AREA AT LEFT FUSELAGE LOWER FAIRING SKIN COMMON TO HORIZONTAL STAB LOWER BLADE SEAL APPROXIMATELY STASDR CALA2015072400607Frame · crackedBELL FRAME AT BS 1580 HAS CRACK AT INBD FASTENER LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8L & 9L. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.SDR CALA2015072400606Frame · crackedCABIN FRAME CRACKED AT STATION 760 AT PSU RAIL BRACKET INBD FASTENER BETWEEN STRINGER 7R & 8R. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.SDR CALA2015072400604Skin · crackedR1 DOOR INTERIOR SIDE, HAS CRACK AT LIGHTNING HOLE, TOP END, UNDER DOOR SLIDE FWD ATTACH BRACKET. COMPLIED WITH ECRA 5210-02655. SEE WIPS FOR ALL WORK ACCOMPLISHED.SDR CALA2015072400601Frame · crackedBELL FRAME AT BS 1540 HAS CRACK AT INBD FASTENER LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8L & 9L. INSTALLED REPAIR IAW SRM 53-00-07 REPAIR 1.SDR CALA2015072400599Floorbeam · corrodedFORWARD WET AREA, STATION 345 FLOORBEAM IS CORRODED FROM BL0 - 24L. REPAIRED FLOORBEAM UPPER CAP STATION 345 BETWEEN LBL 58 & RBL 60 IAW SRM 53-00-51 REPAIR 10 & ECRA 5310-06539.SDR CALA2015072400603Frame · crackedBELL FRAME AT BS 1580 HAS CRACK AT INBD FASTENER, LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8R & 9R. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.SDR CALA2015072400602Frame · crackedBELL FRAME AT BS 1540 HAS CRACK AT INBD FASTENER, LOCATED AT PSU SUPPORT BRACKET BETWEEN STRINGER 8R & 9R. INSTALLED REPAIR IAW SRM 53-00=07 REPAIR 1.SDR CALA2015072400597Floorbeam · corrodedMID WET AREA, STATION 720 FLOORBEAM IS CORRODED, BETWEEN RT INBD & OTBD SEAT TRACKS. REPAIRED MID WET AREA IAW ECRA 5310-06546 & SRM 53-00-51.SDR CALA2015071700580Skin · dentedREINSPECTED DENT AFT CARGO DOOR SKIN 7.5" ABOVE LOWER EDGE & 8.5" FROM AFT EDGE. FOUND DIMENSIONS AS FOLLOWS A=1.7"Y=.059" A/Y=28.81 OUT OF LIMITS. REPAIRED DENT IAW SRM 52-30-01 REPAIR 4.SDR CALA2015071700579Pump · failedDURING CLIMB FROM FL360 TO FL380, LT HYD QTY WENT FROM FULL TO ZERO WITHIN A SECOND. COMPLETED QRH CHECKLIST. ON ARRIVAL, FLEW APP & LOST PTU, NORMAL LANDING. R & R NR 1 EDP HYD & HOSE PN AE709566-1 IAW MM 29-11-05. OPERATIONS & LEAK CHECKED GOOD.SDR CALA2015071700577Floorbeam · corrodedCABIN FLOORBEAM STATION 365 BETWEEN RBL 6 TO RBL 19, CORROSION. REMOVED CORROSION AT CABIN FLOORBEAM STATION 365, BL0 TO RBL 24.75 .027. REMOVED RBL 10.25 & .014, REMOVED AT RBL 14.25 FROM .125 THICKNESS FOR CLEANUP & IS OUT OF LIMITS. ALL OTHER BLEND AREASSDR CALA2015071500572Unknown · engagedLOW SPEED ABORT AROUND 80 KTS FOR RT THROTTLE. AFTER AUTO THROTTLE ENGAGED RT THROTTLE STOPPED HALFWAY & WOULD NOT MOVE. DISENGAGED AUTO THROTTLE, STILL WOULD NOT MOVE FWD, RT THROTTLE RETURNED TO IDLE. FOUND NR 2 ENG PART POWER BAULK ENGAGED. STOWED BAULKSDR CALA2015071500567Unknown · malfunctionedFOR SDR REPORTING, LOW SPEED ABORT UNDER 20 KTS ON TAKEOFF, AUTO THROTTLE ISSUE. DEFERRED LOG PAGE 7495441 INBD TAKEOFF. WHEN AUTO THROTTLES SELECTED, LT THROTTLE DIDN’T RESPOND. COLLARED CB F16 TMC SERVO.SDR CALA2015071400560Control Box · unserviceableAFTER LANDING, WHILE ATTEMPTING TO CROSS RUNWAY, IT TOOK UNUSUALLY HIGH AMOUNT OF POWER TO TAXI ACFT. NOTICED RT SIDE BRAKE TEMP 3 & CONTINUED TO CLIMB, STOPPED ACFT & CALLED MX FOR ASSISTANCE. FOUND ANTI-SKID, ANTI-BRAKE CONTROL BOX WITH BOA AB FAULT & RT ISDR CALA2015071400558Hydraulic Line · rupturedCOMPLETE LOSS OF LT HYD, FOUND RT LG DOWN LOCK ACTUATOR HYD LINE LEAKING. REPLACED HYD LINE IAW AMM 20-10-10-401. LEAK CHECKED LINE, NO LEAKS FOUND. NEW HYD LINE INSTALLED MFG NR IS 271N6119-1.SDR CALA2015070200549Frame · crackedCABIN FRAME CRACKED STATION 760 AT PSU RAIL & BRACKET INBD FASTENER BETWEEN STRINGER 7L & 8L. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 1 PAR 4 STEPS A - S. IMITATED DIP TO PERFORM DETAIL VISUAL INSPECTIONSDR CALA2015070200548Floorbeam · corrodedFORWARD WET AREA FLOORBEAM AT STATION 365 FROM BL 0 TO BL 10R IS CORRODED. IAW ECRA 5310-05536 FABRICATED & INSTALLED ALL REPAIR PARTS & ANY ADJACENT STRUCTURE THAT WAS DISPLACED TO FACILITATE REPAIR. CORROSION INHIBITING COMPOUND TO BE APPLIED DURING WET ARSDR CALA2015062900532Switch · defectiveCLIMBING DURING FL 190 GOT LE SLAT ASYM EICAS MSG WITH A LE DISCRETE LIGHT. RAN THE CHECKLIST & COMPLIED. CLEARED OFF AT FL 2101 THEN WENT BACK DOWN TO FL 200 235 KTS HAD NO CONTROLLABILITY PROBLEMS TS IAW FIM 27-5100-815-805. FOUND FAULT SLAT LOSS MSG 317 SDR CALA2015062400527Ratio Changer · leakingREF LOG PAGE 8279019, LT HYD QTY LOW IN FLIGHT. FOUND RUDDER RATIO CHANGER LEAKING. R & R SAME IAW MM 27-21-13. OPERATIONS & LEAK CHECKED GOOD.SDR CALA2015062200522Floorbeam · corrodedFLOORBEAM AT STATION 1640 BETWEEN RBL-54 & RBL-57 CORRODED ON TOP SIDE. REPAIRED FLOORBEAM STATION 1640, LBL 11 - RBL 65 IAW SRM 53-00-51 REPAIR 8.SDR CALA2015061900520Controller · faultyFOR SDR REPORTING REF LOG PAGE 8141931. AUTO BRAKE DISENGAGED ON LANDING. WHEN MANUAL BRAKES APPLIED ACFT PULLED HARD LT. GRABBED ALSO AT GATE TURN IN. ACCOMPLISHED FIM 32-42-00-815-805 & ACP AMM 32-41-00-825-018. CHECKED BRAKE SYS. REPLACED ANTISKID & ASDR CALA2015061600516Hydraulic Line · rupturedFLIGHT RETURNED DUE TO ZERO HYD QTY ON LT HYD SYS. SYS SHUTDOWN & EMER DECLARED. NOSE WHEEL STEERING AFFECTED. FOUND FWD FLEXIBLE LINE ON RT MLG DOWN LOCK ACTUATOR RUPTURED. INSTALLED NEW MLG FLEX LINE, SERVICED HYDS, BLED SYS & PERFORMED OPERATION CHECKS SDR CALA2015061600514Warning System · false activationTE FLAP DISAGREE LIGHT & EICAS MSG. FLAPS STUCK AT 20. PERFORMED FLAP & SLAT FSEU BITE IAW FIM 27-51-00-815-805. GOT NR 1 FSEU MSG 305. PERFORMED TE & FLAP OPERATIONS CHECK IAW 27-51-00-862-004 & FIM 27-51-00-815-818, FAULT MSG CLEARED. ELEX 1, 2 & 3 NO EXSDR CALA2015061500512Hydraulic Line · rupturedREFERENCE LOG PAGE 8047966. LT HYD SYS LEAKED TO ZERO. FOUND FWD FLEXIBLE LINE ON RT MLG DOWN LOCK ACTUATOR RUPTURED. INSTALLED NEW FLEXIBLE LINE, PN 19-3232-3-0067. REFERENCED IPC 32-32-51-15 ITEM 270. SERVICED LT HYD SYS TO 48%.SDR CALA2015061500510Pan · wornAFT CARGO DOOR LOWER SIDE OF DOOR PAN WORN IN SEVERAL AREAS & TEFLON PAINT WORN OFF. AFT CARGO DOOR LOWER SIDE PAN & TEFLON PAINT ADDRESSED IN PREVIOUS WIPS AS REQUIRED LEVELING COMPOUND IAW AMM 51-41-00-352-013. CURE TIME COMPLIED WITH ALSO CLOSED AREA OPENSDR CALA2015061500509Beam · wornLOWER CTR SECTION OF DOOR PAN ON FWD CARGO DOOR WORN IN 2 SPOTS & TEFLON PAINT WORN AWAY. AREA PAN THAT MAKES CONTACT WITH PRESS SEAL, THE LOWER CTR SECTION OF DOOR PAN OR BEAM WAS REPLACED PN 1 REPAIRED IAW ECRA 5230-01969. DAILY INSPECTION REQUIRED WITH PESDR CALA2015061100501Flap · damagedRIGHT INBD FLAP HAS 2 EACH ELONGATED FASTENER HOLES, LOCATED INSIDE PANEL 655AR. REPAIRED 2 EACH RT INBD FLAP FASTENER HOLES IAW ECRA 5750-0 4789 SEE WIPS FOR WORK ACCOMPLISHED.SDR CALA2015061000499Hinge Fitting · crackedNUMBER 1 ENG INBD T/R AFT HINGE FITTING UPPER ATTACH BOLT NR 1 HOLE CRACK INDICATION. CONFIRMED NDT PART 6 SECTION 51-00-16 & 51-00-17 AFTER SECOND OVERSIZE, REF EA 5451-01040 REV A STEP 4.3. REPAIRED FASTENER LOCATION IAW ECRA 5451-01176.SDR CALA2015061000498Skin · dentedSKIN DENTED FROM INSIDE OUT BS 375 BELOW STRINGER 22R DIMPLE PROTRUDES OTBD. CUT OUT DAMAGED AREA. FABRICATED & INSTALLED REPAIR IAW SRM 53-00-01 REPAIR 7 FIG 201.SDR CALA2015061000496Hydraulic System · lowHYDRAULIC QTY 0.57 RF LT SIDE. EICAS HYD QTY ON APPROACH. SERVICED LT HYD SYS IAW AMM 12-12-01-301. PRESSURIZED LT HYD SYS IAW AMM 29-00-00, NO LEAKS NOTED.SDR CALA2015060400485Stringer · damagedLEFT FUSELAGE, AFTER PREVIOUS REPAIR REMOVED, FOUND STRINGER 17LT BETWEEN STATION 600 & 620 HOLES ARE DAMAGED & DIMPLED ON OUTER SURFACE. INSTALLED REPAIR CHORD IAW AVO IAH043015-0101-1A & ECRA 530 0-02178.SDR CALA2015060400484Skin · cracked4R DOOR HAS A CRACK ON LIGHTNING HOLE 4TH HOLE FROM TOP. REPAIRED 4R DOOR IAW ECRA 5210-02624.SDR CALA2015060400483Frame · wornAFT FUSELAGE FRAME WORN AT STATION 1640, BELOW STRINGER 5R. REPAIR OF AFT FUSELAGE FRAME AT STATION 1640 BETWEEN STRINGER 5R & 6R IAW ECRA 5310-06504.SDR CALA2015060100461Battery Pack · dischargedEMERGENCY LIGHTS AT FIRST CLASS SEATS ARE INOPERATIVE. REPLACED EMER LIGHT BATTERY PACK M731. PERFORMED AN OPERATIONAL TEST, FOUND NORMAL IAW AMM 33-51-07.SDR CALA2015052900456Oven · unserviceableOVEN 413 IN AFT GALLEY PRODUCED WHITE SMOKE AT START-UP, FLIGHT ATTENDANT DISCONTINUED USE. R & R OVEN 413 AFT GALLEY. OPERATIONS CHECKED SEVERAL TIMES. OPERATIONS CHECKED NORMAL & NO SMOKE NOTED. AMM REF 25-34-00-000-801C3 & 25-34-00-400-801C1.SDR CALA2015052100416Light · inoperativeSEAT EMER LIGHTS INOPERATIVE ROW 20 TO 30. REPLACED LIGHT ASSEMBLY AT ROW 20 & PACK FUSES OPERATIONS GOOD. REF LOG PAGE 8173409, REPLACED SPLICE UNDER SEAT 30 EMER EXIT.SDR CALA2015052100411Actuator · inoperativeREF EA 3520-01329 REV B FOUND FWD LAVATORY OXYGEN MASK DOOR ACTUATOR INOPERATIVE. R & R FWD LAVATORY OXYGEN MASK DOOR ACTUATOR IAW AMM 35-21-06. OPERATIONS CHECKED GOOD.SDR CALA2015052100410Doubler · dentedLARGE DENT ON EXISTING FUSELAGE SKIN DOUBLER AT STATION 620 & STRINGER 16L. REMOVED DAMAGE FROM STATION 590 - 650, STRINGER 13L - 20L, REPAIRED IAW SRM.SDR CALA2015051800405Structure · crackedCRACK ON L4 DOOR OUTER CHORD, 146N6100-59, IN RADIUS AT APPROX STATION 1669 AT DOOR HANDLE PAN CUT-OUT. R & R CHORD IAW SRM 51-40-02 & DWG 146N6100.SDR CALA2015051800402Stringer · damagedLEFT FUSELAGE AFTER PREVIOUS REPAIR REMOVED, FOUND STRINGER 15L FROM STATION 600 - 630 ALL THE HOLES ARE DIMPLED ON OUTER SURFACE. REMOVED & REPAIRED DAMAGED STRINGER 15L IAW SRM 53-00-03.SDR CALA2015051800401Stringer · damagedRIGHT SIDE FUSELAGE, STRINGER 16LT, DAMAGED, DENTED BETWEEN STATION 620 - 640. DAMAGED FOUND AFTER PREVIOUS REPAIR REMOVED. R & R DAMAGED STRINGER 16L IAW SRM 53-00-03.SDR CALA2015051500400Frame · crackedCABIN FRAME STATION 800 IS CRACKED AT FASTENER BETWEEN STRINGER 8R & 9R. FABRICATED & INSTALLED REPAIR CHANNELS 1 & 2 AT STATION 800 BETWEEN STRINGER 8R & 9R IAW SRM 53-00-07.SDR CALA2015051500387Oven · dirtyFOR SDR REPORTING, SDR REPORTED FOR SMOKE FROM OVEN. FOOD RESIDUE, OVEN PLACARDED.SDR CALA2015051100384Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION STATION 365 BL-0 THRU 45 APPROX. REMOVED CORROSION AT CABIN FLOORBEAM, MATERIAL REMOVED FROM ORIGINAL .125 & THICKNESS RBL22.25. DAMAGED CLEANED UP & IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-51. DAMAGE IS LIMITED TO EXISDR CALA2015050600374Frame · crackedCABIN FRAME CRACKED AT PSU RAIL BETWEEN STRINGER 8R & 9R. REPAIRED CABIN FRAME AT STATION 760 BETWEEN STRINGER 8R & 9R IAW SRM 53-00-07. REPAIR ONE DETAIL ONE PLACED ON DIP TO DO DETAIL VISUAL INSPECTION OF REPAIR AT 12000 FLIGHT CYCLES OR 50000 AIRFRAME FLISDR CALA2015050600371Frame · crackedCABIN FRAME IS CRACKED AT FASTENER, STATION 1580 BETWEEN STRINGER 8 RT & 9 RT. REPAIRED CABIN FRAME IAW SRM 53-00-07 REPAIR 1.SDR CALA2015050600369Pan · damagedMAIN PAX DOOR L1 NOTED HANDLE PAN NOTED DAMAGED. R & R PAN AT L1 DOOR IAW SRM 51-40-02 & DWG 141N6100.SDR CALA2015050400367Coffeemaker · sparksREAR RT COFFEE POT HAD SHOWN SPARKS, CB`S IN GALLEY PULLED. FORM 46.6020 COMPLETED BY FLT CREW & ATTACHED. COMPLIED WITH AMM 05-51-58 WITH COFFEEMAKER AT 416 AT FAULT. REPLACED BOTH COFFEEMAKERS 416 & 415 AS PRECAUTION. OPERATIONS NORMAL WITH NO OTHER DISCSDR CALA2015050400363Fuse · inoperativeLEFT EXTERNAL FUSELAGE EMERGENCY LIGHT, AFT OF LT WING, INOPERATIVE. REPLACED THE FUSE IN THE POWER SUPPLY & OPS CHECKED NORMAL IAW WD 33-51-14 AMM 33-51-00.
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