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 CALA2019093001667Skin · corrodedB757-06-3-0221 LAVATORY SERVICE PAN BULGING OUT WITH INDICATION OF CORROSION BETWEEN PAN AND SKIN FROM STA 1540-1560 STR 29R-27R . REF ST-ENG N/R 0071138 ACCOMPLISHED ECRA 5331-02469 REV - PART 1 INTERIM REPAIR ON FUSE LAGE SKIN AT LAV SERVICE PAN SKIN CUT OUTSDR CALA2019093001666Frame · corroded(CUSTOMER REQUEST) SECONDARY FINDING AFTER AFTER REMOVAL OF THE AFT LAV SERIVICE PAN AT STA 1560 FOUND THE FRAME CORRODED AT STA 1560 STR 29R. REF ST-EMG N/R 0078792. ACCOMPLISHED REPAIR PER ECRA 53111-02259 PART 1 INTERIM REPAIR O N FRAME B.S 1560 BTWN S28R ASDR CALA2019093001663Skin · corrodedFROM CUSTOMER PICKUP SHEET EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND AFT SIDE AND BETWEEN LAV SERVICE PAN AT STA 1560 STR 27R TO STR 29R. REF ST-ENG N/R 0078758 ACCOMPLISHED PERMANENT REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN STA 1540-1560 R/H ST STRG 26R-30RSDR CALA2019100701713Fitting · defectiveREFRENCE ECRA 5451-01206 #1 ENGINE O/B HINGE FITTING HOLE #3 BOR E WEAR - INTERM REPAIR. CONTACT ENGINEERING AFTER 22 MONTHS AND BEFORE 23 MONTHS FROM TH E DATE OF THE 8100-9/ AMOC TO BEGIN COORDINATION ON PERMANENT UP PER CHORD/SPAR WEB REPAIR. NOTE TO ENGINESDR CALA2019092701639Support Angle · cracked(B757-06-3-0354) FWD CARGO DOOR FWD AND AFT CORNER UPPER SUPPORT ANGLES ARE CRACKED AS MARKED (114-01) REF ST-ENG N/R 0071144. REMOVED 2EA CRACKED BRACKETS, FABRICATED AND INSTALLED 2EA BRACK ETS AT FWD CARGO DOOR, FWD AND AFT CORNERS UPPER SUPPORT ANGLES; P/NSDR CALA2019092701633Angle · damaged#2 PYLON UPPER INBOARD ANGLE HAS DISCOLORED PAINT FROM PP STA 153.9 TO THE AFT END. ACCOMPLISHED HEAT DAMAGE EVAUATION IAW AVO7939, SRM 51-20-03, & 757 NTM PART6 51-00-18. FOUND HEAT DAMAGE FROM PP STA. 155 TO PP STA. 164. ON I/B ANGLE. LOCKING ITEM FOR FERRYSDR CALA2019092301612Gate · corrodedB757-52-3-0374 R4 DOOR - LOWER GATE SKIN EDGE, ALONG THE RUB STR IP IS CORRODED (MK 033-595) REF N/R 0071408. CHECKED LIMITS TO CORROSION R4 DOOR AT LOWER GATE SKIN EDGE, ALO NG RUB STRIP; L=1.2" W=.30" D=.150". OUT OF LIMITS IAW SRM 52-10-02 FIG 101, DETAIL ISDR CALA2019092301611Frame · corrodedB757-06-3-0221 AFT CARGO STUB FRAME AT STA 1450, AT RT LWR SILL HAS CORROSION AT BOTTOM ON BOTH SIDES OF FRAME. (96-03) REF N/R 0071595 BLENDED AND CHECKED LIMITS ON STUB FRAME WEB AT STA 1450 RT LWR SILL BOTTOM ON BOTH SIDES; L=1.5" W=1.0" D=.010". OUT OF LIMSDR CALA2019092301610Stringer · corrodedB757-06-3-0221 AFT CARGO STR 28R HAS EXFOLIATION CORROSION AT S TA 1560. (96-06) REF N/R 0071598. CHECKED LIMITS TO CORROSION ON STR 28R AT AFT CARGO STA 1560; L =.90" W=.60" D=.085". OUT OF LIMITS IAW SRM 53-00-03 FI G 101, DETAIL II. REPAIRED STRINGER IAW SRSDR CALA2019092301609Stringer Splice · corroded(B757-06-3-0242) AFT CARGO, BILGE AREA STA 1620 29R STRINGER SPL ICE HAS CORROSION AS MARKED 50-014. REF N/R 0071559. CHECKED LIMITS TO STRINGER SPLICE AT AFT CARGO BILGE AREA STA 16 20, S-29R; L=1.5" W=.75" D=.050". OUT OF LIMITS IAW SRM 53-00-03 AD1, FIG 101SDR CALA2019092301608Skin · punctured(SUPPORT EA 5210-01364 REV G SEQ NO.1493) DURING DOOR ADJUSTMENT FOUND INTERNAL WEB PUNCTURED BETWEEN RETRACTABLE DOOR AND ASSIS T HANDLE ON R4 DOOR. REF N/R 0073345 SUBMITTED R4 DOOR AT INTERNAL WEB BETWEEN RETRACTABLE DOOR AND ASSIST HANDLE TO ENGINEERING; LSDR CALA2019092301607Strap · corrodedB757-49-3-8084 APU INLET DOOR HOUSING ASSY TO FUSLAGESTRUCTURE F WD EDGE HAS CORROSION. RL050. REF N/R 0071426. CHECKED LIMITS TO APU INLET DOOR HOUSING ASSY TO FUSELAGE STRUCTURE FWD EDGE; L=2.0", W=1.0", D=.125". OUT OF LIMITS IAW SRM 53-80-15, AD 1, PG 102,SDR CALA2019092301606Crease Beam · corroded(B757-53-3-0556) CORROSION ON MAIN CABIN LT CREASE BEAM INNER CHORD UPPER SURFACE STA 732-735 AS MARKED 50-032. REF N/R 0071663 BLENDED AND CHECK LIMITS TO LT CREASE BEAM INNER SHORD IN MAIN CABIN STA 732-735; L=3.5" W=1.0" A=.014". OUT OF LIMITS IAW SRM 53-30SDR CALA2019092301605Frame · corrodedB757-53-3-0526 AFT CARGO STUB FRAME AT STA 1445, AT RT LWR SILL HAS CORROSION AT BOTTOM ON BOTH SIDES OF FRAME (96-02) REF N/R 0071577 BLENDED AND CHECKED LIMITS TO AFT CARGO STUB FRAME WEB AT STA 1445, RT LWR SILL ON BOTH SIDES; L=2.0" W=3.0" D=.056". OUT OF SDR CALA2019092301598Stringer · crackedB757-53-3-0556 MAIN CABIN STRINGER 16L AT STA 780+36 CRACK AS MARKED 034-036. REF N/R 0071602 REPAIRED CRACK AT MAIN CABIN STRINGER AND AT STA 780+36, S-16L; L=.700". IAW ECRA 5340-01884. NO FURTHER ACTION REQUIRED, OK TO CLOSE LOGPAGE.SDR CALA2019092301595Pan · chafedB757-52-3-0368 R1 DOOR EXTERNAL HANDLE PAN HAS A CHAFING MARK ( MK 033-606) REF N/R 0071419. CHECKED LIMITS TO CHAFE AT R1 DOOR EXTERNAL HANDLE PAN; L=1.6", W=.450", D=.010". OUT OF LIMITS IAW SRM 52-10-01 AD1, D ETAIL II. REMOVED AND REPLACED EXTERNAL HANDLE SDR CALA2019092301594Stringer · crackedB757-53-3-0559 STRINGER 16R IN MAIN CABIN IS CRACKED AT STA 780+ 24 (96-23) REF ENGINEERING N/R 0073007. REPAIRED CRACK AT MAIN CABIN STA 780+24, S-16R; L=2.0" IAW ECRA NR 5330-06610. NO FURTHER ACTION REQUIRED, OK TO CLOSE LOGPAGE.SDR CALA2019092301593Deck Plate · corrodedB757-53-3-0579 LIGHT CORROSION IN MAIN DECK AFT DECK PLATE UPPER SURFACE AT STA 1681 FROM LBL 45 INCH BETWEEN RBL 54 INCH. REF S T-ENG N/R 0073073. REMOVED CORROSION FROM AFT DECK PLATE STA 1681 LBL 47 TO RBL 54. L=3.3", W=1.35", D=.013 AREA WAS FOUND TO BE OUSDR CALA2019091401536Stringer · cracked5757-53-3-0556 STRINGER 16L IN MAIN CABIN IS CRACKED AT STA 780+ 36 (96-22) REF ST ENGINEERING N/R 0073006 REPAIRED 1.5" CRACK AT STRINGER 16L IN MAIN CABIN STA 780+36 IAW ECRA 5330-06607.SDR CALA2019091401535Stringer · crackedB757-53-3-0559 STRINGER 16R IN MAIN CABIN IS CRACKED AT STA 780+ 36.(96-24) REF ST ENGINEERING N/R 0073008 REPAIRED 2.0" CRACK AT STRINGER 16R IN MAIN CABIN STA 780+36 IAW ECRA 5330-06608.SDR CALA2019091401534Duct · damaged1/2 L ENG OVHT EICAS AND MSG AND LIGHT CAME ON. ALL ENG PARAMETERS WERE NORMAL. PER CONVERSATION WITH THE CAPTAIN, THE OVERHEAT EICAS AND PEDESTAL LIGHT WAS ON ENGINE #2. PERFORMED VISUAL INSPECTION OF #2 ENGINE. NO OBVIOUS DEFECTS OF RUPTURED DUCTS, LINES, ORSDR CALA2019091701547Structure · dentedLT ELEVATOR TRAILING EDGE HAS A NICK. REF ST-ENG N/R 0073310 ACCOMPLISHED A PERMENANT REPAIR ON LT ELEV T/E IAW SRM 51-40-02, 51-60-01, 51-70-04, 55-20-01 AMM 51-21-10-377-003 DWG NR 183N2003, 183N2302, 183N2402.SDR CALA2019090901506Floorbeam · corrodedB757-53-3-0551 (SECONDARY FINDING)MAIN CABIN FWD FLOORBEAM AT A PPROX STA 345 RBL 2-LBL 40 HAS CORROSION,16-126 REF ENGINEERING N/R 0073053 REMOVED CORROSION FROM MAIN CABIN FLOORBEAM UPP CAP STA 345 RBL 2 TO LBL 40 (L=22 X W=2 D=.028) FOUND TO BE OUT OF LIMITSDR CALA2019090601498Stringer · crackedB757-53-3-0556 MAIN CABIN STRINGER 16R STA 780+24 CRACK AT END AS MARKED 034-037. REF ST-ENG N/R 0071603. REMOVED, FABRICATED AND REPLACED CRACKED STRINGER AT 16R, STA 780-780+24 IAW SRM 51-40-02 FIG 8 DETAIL II AND DRAWING. AREA FREE OF FOD.SDR CALA2019083001444Stringer · crackedB757-53-3-0556 STRINGER 16L IN MAIN CABIN IS CRACKED AT STA 780+ 24. REF ST-ENG N/R 0073005 REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER AT MAIN C ABIN LH STA 780 TO STA 780+24 STRG 16L IAW B757-300 SRM 51-40-02 PG21 FIG 4 AND BOEING DWG 143N5300. THSDR CALA2019083001442Gate · corrodedB757-06-3-036 L2 DOOR LOWER GATE HAS CORROSION.ID NO 30-031 REF. ST. ENGINEERING N/R 0072779 REMOVED CORROSION AT L2 DOOR LWR GATE IAW B757-300 SRM 52-10-02 FIG 101 PG 103. MECHANICALLY MEASURED AREA WITH TOOL ID 13-1323 DATE DUE 10JUN20. FOUND AREA OT BE OUT SDR CALA2019082601433Gate · corrodedB757-06-3-0358 L1 DOOR LOWER GATE HAS CORROSION ID NO 30-017 REF REMOVED CORROSION AT L-1 DOOR LWR GATE IAW SRM 52-10-02 FIG 101 PG 103. FOUND AREA TO BE OUT OF LIMITS IAW SRM 52-10-01. REMOVED AND RE PLACED L1 DOOR LOWER GATE.SDR CALA2019072401241Wire · openFOUND FOWARD EXIT SIGN AT DOOR 3 RIGHT INOP REMOVED CEILING PANEL ABOVE DOOR 3 RIGHT FOR TROUBLESHOOTING AND REMOVED DADO PANEL JUST AFT OF DOOR 3 RIGHT RANG OUT BOTH WIRES ON LIGHT FORWARD FOR DOOR 3 RT AND FOUND AN OPEN ON GROUND WIRE REF AWD 33-51-22, PG 90SDR CALA2019072401236Idg · inoperativeL GEN KICKED OFF INFLGHT FOLLOWED QRH. RESET ONCE KICKED OFF AGAIN. REMOVE THE CONNECTOR BACKSHELL AND INSPECT THE WIRES IF THE ABOVE LOOKS GOOD, THEN DISCONNECT D1014P AT THE PYLON DISCONNECT AND INSPECT CONTACTS 3,12,13 AND 14 FOR DAMAGE NECTOR AND INSPECT TSDR CALA2019071501196Skin · dentedB757-06-3-0380 EXTERNAL FUSELAGE REPAIR HAS DENT AT APPROX. STA 612,ON STGR 17L,16-6 REF. ST. ENGINEERING N/R 0065099 INITIATE A DTA DIP/LP TO ACCOMPLISH INSPECTION REQUIREMENTS ON O R BEFORE THE A/C REACHES 67600 TOTAL A/C FLIGHT CYCLES. PLANNING TO CONTACT ESDR CALA2019070801164Stringer · crackedB757-53-3-0556 MAIN CABIN SRT 16L AT STA 780+40 IS CRACKED FROM EDGE TO FASTENER. (APP .5 INCH) REF ST-ENG N/R 0065402. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE/STRINGER AT S-16L AND STA 780+40 PER EC/RA 5330-06573 REV - .SDR CALA2019070801163Stringer · crackedB757-53-3-0556 MAIN CABIN STA 780+20 STR 16L CRACKED FROM EDGE TO FIRST FASTENER. (APP. 5 INCH) REF ST-ENG N/R 0065401 ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE/STRINGER 16L AT STA 78 0+20 PER EC/RA 5330-06578 REV -.SDR CALA2019070801158Frame · gougedB757-53-3-0261 MAIN CABIN FRAME STA 1280 BETWEEN STR 14R AND 11R HAS THREE GOUGES ON FRAME WEB. REF ST-ENG N/R 0065532. ACCOMPLISHED INTERIM REPAIR AT MAIN CABIN FRAME STA 1280 BETWEEN STGR 11R AND STR 14R IAW ECRA 5360-01526, SEE LOGPAGE 3 680636 FOR REPETETISDR CALA2019070801154Longeron · crackedB757-53-3-0556 LONERON 16R AT STATION 780+40 IS CRACKED ON ITS END. REF ST-ENG N/R 0065379 ACCOMPLISHED PERMANENT REPAIR BETWEEN FUS. STA 780-36 TO STA 780 +40, STR 16R IAW EC/RA 5330-06572. WORK WAS ACCOMPLISHED ON ST-ENG N/R 0065379 NO FURTHER ACTION REQUIRSDR CALA2019070301119Longeron · crackedB757-53-3-0556 LONGERON 16R AT STATION 780+20 IS CRACKED ON ITS END. REF ST-ENG N/R 0065378. ACCOMPLISHED PERMANENT REPAIR AT STA 780+20, STR 16R IAW EC/RA 5330-06576 REV-. WORK WAS ACCOMPLISHED ON ST-ENG N/R 00653 78 AND INSPECTION COMPLETED AND ACCEPTED BY SSDR CALA2019070201114Ring · brokenEA 7830-02252 REV A. DURING THRUST REVERSER INSPECTION FOUND NR 2 ENGINE I/B T/R NR9 CASCADE BROKEN- MISSING AND SUPPORT RING BROKEN WITH PARTS MISSING. REF ST-ENG N/R 0065467. REMOVED AND INSTALLED NR 2 ENG I/B T/R CASCADES SEGMENTS IAW AMM 78-31-05-404, DISCSDR CALA2019070301116Gate · corrodedSUPPORT TASK EA 5210-01360 REV J L1 DOOR LOWER GATE HAS MULTOPLE AREAS OF CORROSION AS MARKED 034-047. REF. ST. ENGINEERING N/R 0065757 REMOVED & INSTALLED NEW L1 DOOR LOWER GATE IAW SRM 51-4 0-02 PG. 21,FIG. 4 AND DWG NO. 141N6120. MATERIAL REMOVAL DIMENSIONSSDR CALA2019070201109Ring · missingPDA 1 DURING INITIAL INSPECTION DURING 4C CHECK AT SAT FOUND #2 ENG. I/B T/R #9 CASCADE BROKEN/MISSING AND SUPPORT RING BROKEN.SDR CALA201906301083Duct · leakingACFT AT 18,000 FT, LEFT ENGINE OVERHEAT LIGHT ILLUMINATED. PER QRH, PULLED BACK THROTTLE TO 1.5 EPR AND BLEED OFF. OVERHEAT LIGHT EXTINGUISHED. REMOVED 3 DUCTS. COVERED ALL DUCTS, AIRCRAFT SIDE. PERFORMED LEFT ENGINE UPPER PYLON STRUT LEAK CHECK AND FOUND HOT SDR CALA2019062211004Floorbeam · corrodedB757-53-3-0480 CORROSION ON MAIN CABIN FLOOR BEAM UPPER SURFACE AT STA 680 RBL-53 REF. ST. ENGINEERING N/R 0065606 FOUND CORROSION OUT OF LIMIT IAW B757-300 SRM 53-30-51 L=1.3,W=. 8,D=.037 ON CABIN FLOOR BEAM AT STA 680 RBL 53 AND ACCOMPLISHED PERMANENT REPAIRSDR CALA2019062210979Angle · corrodedB757-49-3-8084 HEAVY CORROSION BETWEEN APU AIR INLET DOOR HOUSIN G ASSY AND FUSELAGE CUTOUT SUPPORT STRUCTURE LANDING RL062 REF. ST.ENGINEERING N/R 0065354 REMOVED CORR ON APU FWD STRAP UPPER & LWR ANGLE,AND REAR MIDDLE STRAP OF THE APU INLET CUT OUT AT STA 18SDR CALA2019062401049Seal Depressor · dentedB757-52-3-0001 FWD CARGO DOOR AFT SEAL DEPRESSOR HAS TWO DENTS,1 6-14 REF. ST. ENGINEERING N/R 0065107 REMOVED & REPLACED SEAL DEPRESSOR ON AFT SIDE OF FWD CARGO DOOR IAW B757-300 SRM 51-40-02 PG. 2-6 & PG. 31-32 FIG.8 DETAIL 2 BOE ING DWG NO. 143N6603 REV. B.SDR CALA2019062401048Crease Beam · corrodedCORROSION ON MAIN CABIN LH CREASE BEAM INNER CHOR D UPPER SURFACE FROM STA 730-755 LBL-64 RG30 REF. ST. ENGINEERIN G N/R 0065600 REMOVED & REPLACED L/H CREASE BEAM INNER CHORD AT L2 DOOR SURROU ND IN MAIN CABIN AT STA. 663 TO 757,LBL 65 IAW BOEING DWG NO 143 NSDR CALA2019061400926Deck Plate · corrodedB757-53-3-0480 CORROSION ON AFT CABIN FLOOR DECK PLATE UPPER SUR FACE FROM STA 1680-1720 BLO TO LBL-54 RG2 REF. ST. ENGINEERING N/R 0065562 REMOVED CORROSION AT MAIN CABIN DECK PLATE STA 1680-1720 BLO TO LBL 54 ORIGINAL MATERIAL THICKNESS 15.071 MAT.LOSS.007 ASDR CALA2019061000912Frame · corrodedCORROSION ON AFT CARGO FRAME FWD SIDE AROUND SHEAR TIES, BRACKETS AND STR CLIPS AT STA 1440 BETWEEN STR 28L-29R. R EF ST-ENG N/R 0063844 LIMITS (L=7.0" W=4.0" D=.025) IAW B757-300 SRM 53-00-07 ALLOW. D MG 1 FIG 101 DET II. FABRICATED AND INSTALLED INTERIM REPASDR CALA2019060430874Housing · gougedR2 DOOR EXTERNAL HANDLE PAN GOUGE AS MARKED 034-052 OFF A/C PART. REF ST-SAA NR 0064108. GOUGE ON R2 DOOR EXT HANDLE PAN (DEPTH WAS .020, MAX ALLOWABLE I SRM 52-10-01 ALLOW DMG 1 FIG 101 DET VI. REMOVED AND REPLACED WI TH NEW PAN PN 654N0243-45 IAW B757-300 SRSDR CALA2019053100870Frame · dentedB757-06-3-0243 DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 1440 ABOVE STR 26L RG7 REF. ST.ENGINEERING N/R 0063855 AFT CARGO FRAME UPPER FLANGE DENT AT STA 1440 STR 26L FOUND TO BE OUT OF LIMITS (L=1.1" X W=1.0" X D=.040")IAW SRM 53-0 0-07 FIG 101.CUT OUT DAMAGSDR CALA2019053100869Angle · corrodedB757-49-3-8083 APU AIR INLET DOOR HOUSING CUTOUT SURROUNDING EDG E HAS CORROSION PUSHING UP SEALANT. REF ST-ENG N/R 0063617 REMOVED CORROSION FROM APU AIR INLET HOUSING CUTOUT EDGE, LOWER ANGLE STA 1787.45-1825, S-6R AND FWD STRAP AT STA 1787.45. S-3R AND S-6RSDR CALA2019060700886Skin · dentedB757-06-3-0222 LOWER FUSELAGE EXTERIOR SKIN DENT AT APPROX. STA 650, BETWEEN 27L AND 26L, 16-8. REF ST-ENG CARD NO 0063664. SKIN DENT AT STA 650 BETWEEN STR 26L AND STR 27L(L=1.35", W=.90" , D=.060")FOUND TO BE OUT OF LIMITS IAW B757-300 SRM 53-00-01 AL LOW DMSDR CALA2019052700845Stringer · crackedB757-53-3-0556 CRACK ON STR 16L AT STA 780+35 FROM EDGE OF STR TO FIRST FASTENER HOLE. REF ST-ENG N/R 0064014 REPAIRED CRACK ON EDGE OF STRINGER TO FIRST FASTENER HOLE ON STR 16L AT STA 780+35 IAW ECRA 5310-07614. WORK ACCOMPLISHED ON NR 0064014.
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