Boeing 757-33N
Service difficulty reports · 1,195
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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 = '75733N' 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 = '75733N' 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 CALA2021031900332Floorbeam · corrodedB757-53-3-0551 FLOOR SUPPORT BS 338 LBL24 HAS CORROSION. REF H AECO GSO NR 9281263SDR CALA2021031600323Floorbeam · corrodedB757-53-3-0579 RH OTBD FLOORBEAM HAS LIGHT CORROSION AT BS1640 RB 44 - RBL 46 REF HAECO GSO NR 9281257 CLEANED AREA ON FLOORBEAM AT BS1640 RBL 44-46 REMOVED .025" ORIGINAL .070", REMAINING .045" FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-52, REMOVED AND REPLSDR CALA2021031200312Floor Support · corrodedB757-53-3-0551 FLOOR SUPPORT BS338 LBL22 HAS CORROSION REF HAE CO GSO NR 9281262 BLENDED AREA ORIGINAL .050" REMOVED .027 REMAINING .023 FOUND TO BE OUT OF LIMITS PER B757-3 SRM 53-00-51 AND BAC 1500-6232. REM OVED AND REPLACED FLOOR SUPPORT PER B757-3 SRM 51-SDR CALA2021031000284Skin · dentedSUPPORT TASK - LEFT WING #3 SLAT SKIN IS DENTED AT O/B AUX TRACK ACCOMPLISHED DOUBLER REPAIR OF #3 SLAT IAW B757-300 SRM 57-43-01, REPAIR 8, FIG 201. PAGE 206 NOTE "C" BLIND FASTENERS IN REPAIR REQUIRE SUPPLEMENTAL REINSPECT 3000 FLT CYCLES AFTER ADD EMP:V8976SDR CALA2021030500257Motor · burnedAC DIVERTED TO DEN WITH SMOKE IN THE COCKPIT. DEBRIEFED CREW AND FROM FILLED OUT. OBVIOUS ELECTRICAL SMELL AND FOUND THE FWD WQU IP COOLING SUPPLY FAN CB POPPED. CREW DID GET THE EQUIPMENT OVHT LITE ON IN FLIGHT AND ON THE GROUND LABOR HOUR UPDATE REPLACED PRISDR CALA2021030300249Shear Tie · corrodedSUPPORT TASK: AFT CARGO STA 1440, FWD AND AFT SIDE ATTACH BRACKE TS CORODED S28R-S29R RECEIVED MAT ID FOR -7 AND -8 SHEAR TIES 7075-0 BARE ALUM IAW BA C WG #146N1101. FORMED NW SHEAR TIES -7 AND -8 IAW BAC DWG #146N 1101. HEAT TREATED 1 EA -7 AND 1 EA -8 SHEARSDR CALA2021030100248Frame · dentedB757-53-3-0496: STA 600 FWD CARGO COMPARTMENT LWR SUPPORT HAS A DENT BETWEEN S25L AND S26L ACCOMPLISHED STA 600 FRAME REPAIR REF EC 5330-06798 PT 1. DIP REQUIRED TO "PERFORM AN INSP PER PT 2 OF ECRA 5330-06798 ON OR BEFORE 30,700 TOTAL AIRCRAFT FC. PLANNING TOSDR CALA2021012700096Connector · damagedDURING CLIMB ABOUT 60NM SOUTH OF KORD AT FL260 RT GEN/AC BUS OFFLINE FOLLOWED BY BOTH UTILITY, DID NOT SEE SMOKE OR A ELECTRICAL SMELL. THE CAPT ALSO STATED THAT HE DID NOT HEAR A CHATTERING SOUND AND BUS POWER CONTROL UNIT BITE OF FAULTED DP TRIP, MAIN BUS OSDR CALA2021012000061Control Switch · inoperativeDURING FLAP RETRACTION RT AC BUS EICAS FOLLOWED QRC RT GEN RESET BUT RT AC BUS REMAINED ISOLATED CREW COMMENTS, RT AC BUS OFF EICAS ON CLIMB AT 5,000 FT. FIRST SWITCH CLOSED, ISOL ILLUMINATED. DURING DEBRIEFING, CAPTAIN OFFICER FOLLOWED QRH WHILE CAPTAIN LEVSDR CALA2021010400008Indicator · no indicationDOOR 1L SLIDE ARMED LGT NOT ILLUMINATED. DOOR 1L ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT, MEL 2566 VERIFIED MEL COMPLIED WITH BY U087244. WITH LIGHT VERTICAL MOVMENT OF FWD END OF GIRT BAR WOULD COME INTO PROX IT APPEARS FWD FITTING NEEDS TO BE ADJUSTED PER ASDR CALA2020101601197Lamp · inoperative1L EXIT LIGHT ABOVE DOOR ONLY 1/2 ILLUMINATED RELAMPED PER AMM 33-51-01-962-001-002 PARTS REPLACED BULB GE OL-3071BPEGPL 6 EA. OPS CHK OK ACP''D IDT INSP. VERIFIED OPERATION OK.SDR CALA2020062501017Slide · partial deployDOOR 2L DOOR WAS DISARMED. AS DOOR OPENED THE SLIDE PACK DEPLOYED BUT DID NOT INFLATE OCED FR FERRY UNLOCK FOR UPDATE AFTER SLIDE FELL OUT OF BUSTLE. REMOVED GIRT BAR AND INSTALLED SAFETY PIN IN INFLATION CYLINDER REF AMM TASK 25-66-01-004-154. SLIDE PACK ISDR CALA2020053100998Stringer · corrodedBULK CARGO COMPARTMENT STR AT RT STATION 1540 TO STATION 1560 STR 29R FOUND WITH EXFOLIATED CORROSION REF N/R 9609453 CUTOUT DAMAGE AREA. FABRICATED AND INSTALLED FUSELAGE STR REPAIR AT STR 29R WITHIN STATION 1520 TO STATION 1580 IAW SRM 53-00-03 REPAIR 1 DETSDR CALA2020052200974Fitting · crackedDURING NDT HFEC ROTO INSPECTION OF NR 1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE 2. REPAIRED HOLE 2 IAW ECRA 5720-031930.SDR CALA2020052200981Fitting · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #1 - CRACK POSITION :- 3:0''CLOCK; CRACK DEPTH :-0.591"; CRACK SIZE :- 0.050" REF AAR NR 9606668 REPAIRED HOLE #1 PER ECRA 5720-03193SDR CALA2020052200978Skin · crackedCRACK INDICATION NOTED ON HOLE # 10 AT R/W PYLON UPPER SKIN DRAG FITTING , CRACK POSITION 2 O''CLOCK , DEPTH APPROX < 0.030" REF AAR NR 9606729 REPAIRED HOLE #10 AT #2 PYLON UPPER DRAG FITTING PER EC/RA 5720-03191.INITIATE A DTA DIP LOGPAGE TO READ AS FOLLOWSSDR CALA2020052200977Skin · cracked2EA CRACKS INDICATION NOTED ON HOLE # 8 AT R/W PYLON UPPER SKIN DRAG FITTING , CRACK POSITIONS 2 O''CLOCK AND 7 O''CLOCK , DEPTH APPROX 0.030" < REF AAR NR 9606727 REPAIRED HOLE #8 AT #2 PYLON UPPER DRAG FITTING PER ECRA 5720-03191 .INITIATE A DTA DIP LOGPAGSDR CALA2020052200976Fitting · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #4 - CRACK POSITION :- 11:0''CLOCK; CRACK DEPTH :-0.500"; CRACK SIZE :- 0.060" REF AAR NR 9606671 REPAIRED HOLE #4 PER ECRA 5720-03193SDR CALA2020052200975Skin · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #10 - CRACK POSITION :- 4:0''CLOCK; CRACK DEPTH :-0.340"; CRACK SIZE :- 0.040" REF AAR NR 9606672 REPAIRED HOLE #10 PER ECRA 5720-0219SDR CALA2020052200980Spar · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #3 - CRACK POSITION :- 3:0''CLOCK; CRACK DEPTH :-0.480"; CRACK SIZE :- 0.050" REF AAR NR 9606670 REPAIRED HOLE #3 PER ECRA 5720-031930SDR CALA2020052200979Skin · crackedCRACK INDICATION NOTED ON HOLE # 9 AT R/W PYLON UPPER SKIN DRAG FITTING , CRACK POSITION 11 O''CLOCK , DEPTH APPROX < 0.030" REF AAR NR 9606728 REPAIRED HOLE #9 AT #2 PYLON UPPER DRAG FITTING PER EC/RA 5720-03191.INITIATE A DTA DIP LOGPAGE TO READ AS FOLLOWSSDR 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 CALA2020042400869Frame · dentedB757-53-3-0523. AFT CARGO COMPARTMENT BS1400 S26L FRAME FOUND W ITH A DENT. MEASURED DENT AT AFT CARGO FRAME STA.1400 S26L FOUND TO BE WITH IN LIMITS IAW B757-300 SRM 53-00-07. INSTALLED DENT DOT ECRA 20 60-01042. LOG PAGE WAS CONVERTED TO ELB FORMAT ON MAY 03SDR CALA2020042400867Stringer · cracked(B757-53-3-0559) STA 780+36 STR 16R CRACKED. REF ST-SAA NR 0091790. REMOVED DAMAGE STR AT STA780+36 STR-16R. ACCOMPLISHED PERMANENT REPAIR IAW B757-300 EC/RA 5310-07781 AT STA 780+36. STR-16R AREA FOD FREE WORK ACCOMPLISHED, INSPECTED.SDR CALA2020042400864Frame · cracked(CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8R AND 9R. REF ST-SAA NR 0092124. CUTOUT CRACK L=1.250 W=1.050 AND INSTALLED PERMANENT REPAIR ON FRAME STA 1580 BETWEEN STRINGER 8R AND 9R IAW B757-3 SRM 53-00-07 RSDR CALA2020042400862Web · cracked(B757-06-3-0374 R-4 DOOR UPPER INNER WEB AFT LIGHTNING HOLE IS C RACKED. REF ST-SAA NR0091847 CHECKED LIMITS TO CRACK AT R4 DOOR UPPER INNER SKIN; L=.25". OUT OF LIMITS IAW B757-300 SRM 52-10-01 ADI, FIG 101 DETAIL XI. ACC OMPLISHED PERMANENT REPAIR IAW ECRA 5SDR CALA2020042400865Frame · cracked(CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8L AND 9L. REF ST-SAA NR 0092123. CUTOUT CRACK 1.180 X 1.040 AND INSTALLED PERMANENT REPAIR ON FRAME STA 1580 BETWEEN STRINGER 8L AND 9L IAW B757-3 SRM 53-00-07-R8 SDR CALA2020042400859Stringer · cracked(B757-53-3-0559) STA 780+24 STR 16R CRACKED. REF ST-SAA NR 0091789. CHECKED LIMITS TO CRACKED STRINGER 16R AT STA 780+24; L=.40". OU T OF LIMITS IAW B757-300 SRM 53-00-53 ADI, FIG 101,NOTE A, NO CR ACKS ALLOWED. REMOVED, FABRICATED AND INSTALLED NEW STRINGER SSDR CALA2020042400858Stringer · cracked(B757-53-3-0560) STA 780+24 STR 16L CRACKED. REF ST-SAA NR 00917 87. CHECKED LIMITS TO CRACKED STRINGER 16L AT STA 780+24 L+.70"; OUT OF LIMITS IAW B757-300 SRM 53-00-03 ADI. NO CRACKS ALLOWED. REM OVED, FABRICATE AND INSTALLED NEW STRINGER 16L SECTION, P/N: VSDR CALA2020041700845Bracket · cracked(B757-06-3-0354) FWD CARGO DOOR UPPER FWD CORNER BRACKET CRACKED . REF ST-SAA NR 0091474. REMOVED AND REPLACED FWD CARGO DOOR UPPER FWD CORNER BRACKET IAW BOEING DWG 143N6603 REV F, NEW BRACKET PN 03-2711-3-0074 BATCH 0003644086. PO NO.TUA00003491. WORK ACCOMPSDR CALA2020041300832Seal Depressor · dented(B757-06-3-0354) FWD CARGO AFT SEAL DEPRESSOR IS DENTED. REF ST- SAA NR 0091477. FOUND FWD CARGO DOOR AFT SEAL DEPRESSOR AT STA 615 S-20R TO S-25 R OUT OF LIMITS IAW B757-3 SRM 52-30-02 FIG 101 REMOVED, LOCATED AND INSTALLED NEW SEAL DEPRESSOR PN 143N6603-105 SDR CALA2020041700838Stringer · cracked(B757-53-3-0560) STA 780 780+36 STR 16L CRACKED. REF ST-SAA NR 0 091788. FOUND STRINGER 16L AT STA 780+36 OUT OF LIMITS IAW B757-3 SRM 53 -30-03-R1 L=.750 CUTOUT DAMAGE AND INSTALLED PERMANENT REPAIR TO STRINGER 16L AT STA 780+36 IAW B757-3 SRM 53-30-03-R1 FIGSDR CALA2020041700837Crease Beam · corroded(B757-53-3-0557) CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE,-LEADING UNDER DRAIN PAN AT L-2 LWR SILL, STA 730-740. R EF ST-SAA NR 0091960. FOUND LH CREASE BEAM INNER CHORD AT STA 660 TO 760 OUT OF LIMITS IAW B757-3 SRM 53-30-15-A1 - FIG 101 L=8 W=1SDR CALA2020041300829Strap · corroded(B757-49-3-8083) APU AIR INLET DOOR HOUSING FUSELAGE CUTOUT HAS CORROSION. REF ST-SAA NR 0091780. REMOVED CORROSION AND CHECKED LIMITS TO APU AIR INLET DOOR HOUSING FUSELAGE CUTOUT FWD STRAP L=3.0 W=1.0 D=.050, OUT OF LIMITS. AFT MIDDLE STRAP L=20 W=1.0 D=.055SDR CALA2020041300828Pan · abnormal(B757-53-3-0545) LH SIDE UPPER LOBE FUSELAGE L1 DOOR HANDLE PAN HAS TWO GOUGES. REF ST-SAA NR 0091391. CHECKED LIMITS TO 2EA GOUGES AT LH SIDE UPPER LOBE FUSELAGE L1 DOOR HANDLE PAN L=2.0 W=.10 D=.012. OUT OF LIMITS IAW B757-3 SRM 52-10-01 FIG 101 DETAIL VI ASDR CALA2020041000802Stringer · crackedB757-53-3-0569. FOUND CRACK AT THE END OF THE STRG 16L AND STA 780+40 +3 IN BY THE EXTERNAL LIGHT ASSY AREA LH SIDE OF THE FUSELAGE AT PASSENGER CABIIN. DOT 82-051. REF AAR NR 9606676 INSTALLED FABRICATED PARTS AT THE END OF THE STRG 16L AND STA 780+40+3IN BY SDR CALA2020041000801Stringer · crackedB757-53-3-0569. FOUND CRACK AT THE END OF THE STRG 16L AND STA 780+40 +3 IN BY THE EXTERNAL LIGHT ASSY AREA LH SIDE OF THE FUSELAGE AT PASSENGER CABIIN. DOT 82-051. REF AAR NR 9606676 INSTALLED FABRICATED PARTS AT THE END OF THE STRG 16L AND STA 780+40+3IN BY SDR CALA2020041000800Stringer · crackedB757-53-3-0569. FOUND CRACK AT THE END OF THE STRG 16R AND STA 780+40 +3 IN BY THE EXTERNAL LIGHT ASSY AREA RH SIDE OF THE FUSELAGE AT PASSENGER CABIN. DOT 82-053. REF AAR NR 9606678 INSTALLED FABRICATED PARTS AT THE END OF THE STGR 16R AND STA 780+40+3 IN BY SDR CALA2020041000799Stringer · crackedB757-53-3-0569. FOUND CRACK AT THE END OF THE STRG 16R AND STA 780+20 -3 IN BY THE EXTERNAL LIGHT ASSY AREA RH SIDE OF THE FUSELAGE AT PASSENGER CABIIN. DOT 82-052. REF AAR NR 9606677 INSTALLED FABRICATED PARTS AT THE END OF THE STGR 16R AND STA 780+20-3IN BY SDR CALA2020040600798Stringer · crackedB757-53-3-0569. FOUND CRACK AT THE END OF THE STRG 16L AND STA 780+20 -3 IN BY THE EXTERNAL LIGHT ASSY AREA LH SIDE OF THE FUSELAGE AT PASSENGER CABIIN. DOT 82-050. REF AAR NR 9606675 INSTALLED FABRICATED PARTS AT THE END OF STRG 16L AND STA 780+20+3IN BY THE SDR CALA2020033000756Solenoid · shortedEICAS MSG. L ENG ANTI-IC E. 5 MIN AFTER SWITCH ACTIVATION REF FIM TASK 30-21-00-815-803 FOUND A/ICE VLV SOLONOID SHORTED. RECCOMEND REPLACING ENGINE A/ICE VLV. PARTS ORDERED TO PARTS DROP. REMOVED #1 ENGINE TAI VALVE PER AMM 30-21-03-004-017. INSTALLED NEW VALSDR CALA2020032100679Shutoff Valve · malfunctionedL ENG BLD OFF NO NO RESPONSE RE CHKLST PREFORMED FIM 36-10-00-815-816, PREFORMED HEALTH CHECK REMOVED A ND REPLACED PRSOV IAW AMM 36-11-07-401 NEEDS HIGH POWER ENG. RUN. VALVE, PNEU, PR OFF 19-3611-9-0004 1061 ON 19-3611-9-0004 1652 ROTABLE PARTS CHANGE WASSDR CALA2020030700602Shear Plate · corrodedAFT CABIN RT SHEAR WEB PLATE HAS SEVERAL EXFOLIATED SPOTS BS 1710-1720 RBL 10-36 8-35 REF AAR N/R 9606234 REMOVED AND INSTALLED NEW DOUBLER P/N 546N5521-2 REF B757 SRM 51-40-02 AND DWG 146N5300-303SDR CALA2020021600438Seal · missingPDA 2 FOUND SEAL MISSING FROM INBD EGDE OF OTBD LH FLAP. RPL''D SEAL REF IPC 57-53-10-51 ITEM 100SDR CALA2020010600100Skin · dentedRAMP REPORTED DENT FORWARD AT 2L DOOR & MEASUREMENTS APPROX 2 INCHES BY 2 INCHES WITH DEEPEST DEPTH AT 3/16 INCHES LOCATED AT APPROX BODY STA 662 & JUST ABOVE W/L 208 BEFORE STRINGER REMOVED DADO PANEL TO INSPECT INTERNALLY, NOTE STRINGER BENT & E VIDENCE OF CSDR CALA2019102301791Connector · damagedDURING CLIMB C HYD QTY DROPPED TO 0 WITH SYS PRESSURE CAUTION LO W INDICATION LOW RSV LIGHT PILOT REPORTED ISSUE OCCURRED AFTER 20 MINUTES OUT BEFORE RETURN TO FIELD. CONTACT TOMC TO UNLOCK AFTER REPAIRS ARE COMPLETE. UNLOCKED FOR UPDATING. CHECKED HI-Z WIRINSDR CALA20191011728Frame · corrodedB757-06-3-0243 AFT CARGO FRAME WEB FWD SIDE STA 1420,28R TO 29; HAS CORROSION, REF ST-ENG N/R 0071526. REMOVED AND CHECKED LIMITS TO CORROSION AT AFT CARGO FRAME WEB F WD SIDE STA 1420, 28R TO 29L, L=5.0" W=3.0" D=.016". OUT OF LIMI TS IAW B757-300 SRM 53-00-0SDR CALA2019100501698Transmitter · malfunctionedFLAP ASYMMETRY EICAS INDICATION AFTER FLAP RETRACTION ON TAKEOFF. RH FLAP NEEDLE STUCK WITH NO FLIGHT CHARACTERISTICS NOTICED. FLAPS INDICATION DID RETURN TO NORMAL ON FLAP EXTENSION FOR LANDING USING NORMAL FLAPS. REMOVED AND REPLACED FLAP POSITION IND. NO JOSDR CALA2019100541684Frame · dentedB757-53-3-0492 FWD CARGO LH FRAME AT STA. 600 AND S-24L HAS A SM ALL DENT AS MARKED. 83-035. REF ST-ENG N/R 0071496. CHECKED LIMITS TO DENT AT FWD CARGO LH FRAME STA 600, S-24L; L=. 60", W=.50", D=.010". OUT OF LIMITSIAW B757-300 SRM 53-00-07, AD 1, FIG 101 ACSDR CALA2019093001674Light · inoperative(MULT-33-3-0001) 01 EACH L2 DOOR AND 02 EACH OVERWING EXTERNAL E MERGENCY LIGHTS INOP. (RELAMP). REF ST-SAA NR 0078793. RELAMPED L2 DR SLIDE LIGHT & OPS CK GOOD REF AMM 33-51-06-962-00 R/R BATTERY CHARGER & BATTERY PACK AT M11383 & 2EA OVERWING EXTERNAL EMERG
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