Boeing 737-4H6
Service difficulty reports · 106
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 = '7374H6' 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 = '7374H6' 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 EE4Y2018030506052Stringer · crackedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT MAIN CARGO CABIN, BETWEEN BS 360 AND 390, THE STRINGER 8L CRACKED, THE DAMAGED STRINGER SECTION WAS REPLACED IAW EO 6072, REV P1.SDR EE4Y2018030506058Skin · dentedDURING THE STRUCTURAL INSPECTION, FOUND AT FWD ENTRY DOOR CUTOUT AREA, BS 332.5 BELOW STRINGER 17L, THE EXTERNAL SKIN WAS DENTED. THE SKIN WAS REPAIRED IAW EO 6070, REV IR.SDR EE4Y2018030506057Stringer · crackedDURING THE INSPECTION PROCESS, FOUND THE FWD CARGO COMPARTMENT, STRINGER 19, BETWEEN BS 400 AND 420, FLANGE WITH TWO CRACKS. THE STRINGER WAS REPAIRED IAW EO 6059, REV IR.SDR EE4Y2018030506061Skin · dentedDURING THE STRUCTURAL INSPECTION, THERE WERE FOUND SEVERAL DENTS AT FWD GALLEY DOOR CUTOUT LOWER SKIN AREA, BS 291.5 AND 344, STRINGER 17R AND 18R. REPAIRED IAW EO 6071.SDR EE4Y2018030506059Skin · dentedDURING THE STRUCTURAL INSPECTION, SEVERAL DEFORMATIONS AND DINGS FROM INSIDE TO OUTSIDE WERE FOUND AT MCD LOWER FRAME SKIN AREA, BS 360 TO 500C, STRINGERS 18L AND 26L. REPAIRED IAW EO 6022.SDR EE4Y2017090304254Stringer Clip · crackedDURING A STRUCTURAL INSPECTION, FOUND THE STRINGER CLIP AT BS 360, STRINGER 10L, CRACKED. THE STRINGER CLIP WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8.SDR EE4Y2017090304261Fitting · damagedDURING THE STRUCTURAL INSPECTION AT THE UPPER FUSELAGE MAIN CARGO CABIN, IT WAS FOUND AT BS 927 STR 17RH, THE FRAME ATTACH FITTING WITH FASTENER HOLE WITH BROKEN SCREW. THE AFFECTED FRAME ATTACH FITTING WAS REPAIRED AS PER AEI E.O.5332 AND APPROVED UNDER FAA 8SDR EE4Y2017090304260Web · corrodedDURING A STRUCTURAL INSPECTION AT THE LT MAIN WHEEL WELL, FOUND SIDE WEB CORRODED, BS 695 - 706, STRINGER 18AL. THE WEB WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8, DRAWINGS 69-78163, AND 65-46877.SDR EE4Y2017090304253Fitting · corrodedDURING THE STRUCTURAL INSPECTION IN THE FWD CARGO BAY AREA, FOUND AT BS 540, THE STRINGER 27L WITH THE END FITTING CORRODED. THE DAMAGED END FITTING WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8.SDR EE4Y2017090104228Shear Web · crackedDURING A STRUCTURAL INSPECTION, FOUND BS 348.2, BETWEEN STRINGERS 16L AND 17L SHEAR WEB CRACKED. THE SHEAR WEB WAS REPLACED IAW SB737-53A1240, WORK INSTRUCTIONS, PART 4, PARAGRAPH F, REV 1, AND EAM3353020-4, SECTION 6.SDR EE4Y2017090104227Attach Angle · crackedDURING A STRUCTURAL INSPECTION, FOUND BS 348.2, STRINGER 15L, AN INTERNAL ATTACH ANGLE FOUND CRACKED. THE ATTACH ANGLE WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS, PART 4, PARAGRAPH C, REV. 1 AND EAM 3553020-4, SECTION 3.SDR EE4Y2017090104226Frame · crackedDURING A STRUCTURAL INSPECTION, FOUND THE BS 348.2FRAME CRACKED AT STRINGER 15L, THE FRAME SECTION WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS PART 4A, REV 1, AND EAM 3553020-4, SECTION 1.SDR EE4Y2017083104206Frame · crackedDURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 500F FRAME WEB WAS FOUND WITH CRACK BETWEEN STR 8L AND STR 9L, SPECIFICALLY AT AC SUPPORT ATTACH BRACKET. MENTIONED DAMAGE WAS REPAIRED IAW SB737-53-1216 PART III FIGURE 8.SDR EE4Y2017083004198Frame · corrodedDURING THE STRUCTURAL INSPECTION AT AIR CONDITION DISTRIBUTION BAY, IT WAS REPORTED AT BS 520 THE FRAME SECTION BETWEEN STRINGERS 27L AND 28L CORRODED. THE DAMAGED FRAME SECTION WAS REPAIRED IAW SRM 53-00-07, FIGURE 201 REPAIR 5.SDR EE4Y2017090304259Channel · corrodedDURING THE STRUCTURAL INSPECTION AT THE LOWER FUSELAGE WATER WASTE PANEL AREA, FOUND THE INNER SIDE CHANNEL CORRODED BETWEEN BS 986 - 1006, STRINGERS 25 - 26R. THE CHANNEL WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8, AND DRAWING 65-55843.SDR EE4Y2017083104207Frame · crackedDURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 727B FRAME WEB WAS FOUND WITH CRACK BETWEEN STRINGERS 8R AND 9R, SPECIFICALLY AT AC SUPPORT ATTACH BRACKET. THE DAMAGE WAS REPAIRED IAW SB737-53-1216, PART III, FIGURE 8.SDR EE4Y2017083104200Frame · crackedDURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 500A FRAME WEB WAS FOUND WITH CRACK BETWEEN STRINGERS 8R AND 9R, SPECIFICALLY AT AC SUPPORT ATTACH BRACKET. REPAIRED IAW SB737-53-1216, PART III, FIGURE 8.SDR EE4Y2017090104229Beam · crackedDURING THE STRUCTURAL INSPECTION, FOUND AT BS 178 RBL 71.1 WBL 226 - 231 THE VERTICAL BEAM WEB CRACKED, THE BEAM WAS REPAIRED IAW SRM 53-10-08, FIG 201, REPAIR 12, DETAIL V.SDR EE4Y201708314210Frame · crackedDURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 727B FRAME WEB WAS FOUND WITH CRACK BETWEEN STRINGERS 8L AND 9L. THE DAMAGE WAS REPAIRED IAW SB737-53-1216, PART III, FIGURE 8.SDR EE4Y2017090304255Spar Web · damagedDURING A STRUCTURAL INSPECTION AT THE RT WING REAR SPAR WEB, FOUND TWO FASTENER HOLES ELONGATED AT RSS 206.11 AND RSS 273. THE ELONGATED FASTENER HOLES WERE REPAIRED IAW S/R 3-3949229341, AND EO COO-EO-2017-3990-R01.SDR EE4Y2017082204133Frame · damagedDURING THE STRUCTURAL INSPECTION, BS 907 FRAME, STRINGER 17L AND 17R, FOUND SEVERAL FASTENER HOLES DAMAGED, THE FRAME AND ATTACHING PARTS WERE REPAIRED IAW EO 5136.SDR EE4Y2017082204076Frame · crackedDURING THE INSPECTION ACCOMPLISHMENT PER EAM3353009-1 REV NR 3 RELATED WITH AD2016-11-04, IT WAS FOUND AT THE LOWER FUSELAGE FWD CARGO COMPARTMENT. STA500G, BETWEEN STR20R AND STR21R FRAME WITH CRACK AT THE 0.500 INCH DIAMETER HOLE. THE AFFECTED FRAME BS 500G SDR EE4Y2017082204079Frame · crackedDURING THE STRUCTURAL INSPECTION OF THE UPPER FWD FUSELAGE IT WAS FOUND AT BS 178 WL 207 THE BULKHEAD LH SIDE CHORD WITH CRACK. THE AFFECTED CHORD HAS BEEN REPLACED IN ACCORDANCE WITH SB 737-53A1208SDR EE4Y2017082204077Skin · canningDURING THE STRUCTURAL INSPECTION OF THE UPPER REAR FUSELAGE IT WAS FOUND THE FUSELAGE SKIN WITH AN OIL CAN AT BS 1006 3 INCH BELOW STRG 16L. THE AFFECTED SKIN AREA HAS BEEN REPAIRED IAW SRM 53-80-01, REPAIR 6.SDR Q2SA20170812384Power Supply · inoperativeDURING AN OPS CHECK OF INTERIOR EMERGENCY LIGHTS, FOUND L1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY, EMERGENCY POWER SUPPLY, OPS CHECKED GOOD IAW AMM 33-51-51. AIRCRAFT GROUNDED.SDR EE4Y2017082204134Skin · crackedDURING INSPECTION, THERE WERE FIVE CRACKS FOUND IN THE UPPER SKIN, T/E AREA BETWEEN RSS 238 AND 267, THE RT WING UPPER SKIN WAS REPAIRED IAW SRM 57-20-01, REPAIR 7.SDR EE4Y2017082204081Skin · crackedDURING INSPECTION, OF THE LT REAR SPAR UPPER CHORD, THERE WERE FOUND THREE CRACKS AT UPPER SKIN T/E AREA, THE AFFECTED LT WING UPPER SKIN AREA WAS REPAIRED.SDR EE4Y2017082204082Spar · crackedDURING THE STRUCTURAL INSPECTION, THE RT WING REAR SPAR WEB AND UPPER CHORD WERE FOUND WITH A CRACK AT RSS 224. THE AFFECTED WEB AND UPPER CHORD SECTIONS WERE REPAIRED IAW SRM 57-20-10, REPAIRS 4 AND 6.SDR EE4Y2017082204080Spar · crackedDURING THE STRUCTURAL INSPECTION THE LT WING REAR SPAR UPPER CHORD WAS FOUND CRACKED AT RSS 223, THE AFFECTED SPAR SECTION WAS REPAIRED IAW SRM 57-20-10, REPAIR 4.SDR Q2SA20170307381Unknown · odorAIRCRAFT GROUNDED. ON CLIMB OUT PASSING 12000 SMELL OF BURNING PAPER WAS NOTICED AND FO EYES IRRITATED. DECLARED EMERGENCY. NO SYSTEM FIRE WARNING. INSPECTED ENTIRE A/C FOR SMOKE / SMELL FLUID STAINS. CHK GOOD OPENED ALL ACCESS PNLS EVERYTHING NORMAL NO SIGNSSDR 7AHR2016080892403Frame · corrodedFS 492.5 FRAME RT HAS CORROSION, REPAIRED FWD PIT DOOR CUTOUT FRAME RT FS 492.5 IAW DWG 5310D2165, REV IR.SDR 7AHR2016080892191Bear Strap · corrodedFORWARD CARGO DOOR JAMB LOWER AFT CUTOUT CORRODED. REMOVED CORROSION ON BEAR STRAP AT AFT CARGO DOOR JAMP IAW SRM 53-00-01, INSTALLED REPAIR ON LOWER FWD CARGO DOOR IAW SRM 53-00-01, REPAIR 32.SDR Q2SA20160728254Stiffener · corrodedCORROSION AFT CARGO BAY FWD BULKHEAD BS 727 BOTTOM OF VERTICAL STIFFENER RBL 19 (FOUND DURING SUPPORT STRAP REMOVAL). AIRCRAFT GROUNDED. REPAIRED IAW SRM 53-60-08.SDR Q2SA20160727253Skin · corrodedWHILE WORKING AFT CORNER CORROSION, FOUND ADDITIONAL CORROSION FWD CARGO DOOR FRAME LOWER AFT CUTOUT. AIRCRAFT GROUNDED. REPAIRED THE DOOR FRAME LWR AFT CUTOUT IAW SRM 53-00-01 REPAIR 33, PB 201-245SDR Q2SA20160727252Filler · corrodedAFT CARGO BAY BS 794.5 UPPER INNER RADIUS FILLER BETWEEN STRINGER 25 & 26R IS CORRODED. REMOVED FILLER, INSTALLED REPAIR IAW DWG 5310021711R. AIRCRAFT GROUNDED.SDR Q2SA20160720250Structure · corrodedAFT CARGO BAY HAS SIGNS OF CORROSION UNDER LEVELING COUMPOUND AT LOWER FWD CORNER OF DOOR CUTOUT. REPAIRED IAW SRM 53-00-01 REPAIR 32 FIG 201. AIRCRAFT GROUNDED.SDR Q2SA20160718249Intercostal · corrodedAIRCRAFT WAS GROUNDED. CORROSION ON INTERCOSTAL FS 472-480, RIGHT STR 26R. R & R INTERCOSTAL FS SRM 51-40-02, PG 6-7.SDR Q2SA20160717248Strap · corrodedACFT WAS GROUNDED. AFT CARGO PIT STRAP AT FS 794.5 RT HAS CORROSION ON TOP SURFACE. REMOVED STRAP & REINSTALLED IAW SRM 51-40-02, FIG 8.SDR Q2SA20160729255Stiffener · corrodedAIRCRAFT GROUNDED. CORROSION AFT CARGO COMPARTMENT FORWARD BULKHEAD STA 727 BOTTOM OF VERTICAL STIFFENER RBBL 10, FOUND DURING SUPPORT STRAP REMOVAL. REPAIRED IAW SRM 53-60-08.SDR Q2SA20160713247Door Frame · corrodedAFT CARGO DOOR HAS SURFACE CORROSION AT LWR AFT CORNER. AIRCRAFT GROUNDED. INSTALLED A NEW AFT DOOR FRAME IAW DRAWINGS 65375475-52A1153 IAW SRM 51-40-02 PG 1-9SDR Q2SA20160713246Shear Tie · corrodedAFT CARGO BAY HAS CORROSION AT BS 947.5 ALONG BOTTOM EDGE OF WALL AND ON THE OTBD SIDE OF S26 - 27L. REMOVED CORROSION & FABRICATED A NEW SHEAR TIE. INSTALLED NEW SHEAR TIE IAW SRM 51-20-01 & 53-00-07 PG 205.SDR Q2SA20160713245Doubler · damagedREPAIR DOUBLER FOUND TO BE OUT OF LIMITS WITH 100% MATERIAL LOSS. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE DOUBLER AND FILLER IAW SRM 51-40-02 FIG 8SDR Q2SA20160724251Floor Panel · corrodedCORROSION ON THE EDGES OF FWD CARGO AFT FLOOR PANEL NR 4 AROUND FASTENER HOLES (PANEL RACK). REMOVED OUT OF LIMIT FLOOR PANEL , FABRICATED A NEW PANEL IAW SRM 51-40-05, 51-30-53, AND 51-20-01. AIRCRAFT GROUNDED.SDR Q2SA20160214242Unknown · smokeON TAKEOFF ROLL, TOWER CALLED SMOKE FROM LT WING REJECTED TO AT 122 KTS. FIRE RESCUE INSPECTION REPORT, NO SMOKE FUEL FROM LT WING. BRAKE ENERGY WAS IN CAUTION RANGE.SDR Q2SA20160208239Attach Fitting · corrodedCORROSION FOUND IN LT HORIZONTAL STABILIZER CENTER SECTION FWD UPPER LUG BORE.SDR Q2SA20160207240Attach Fitting · corrodedLEFT STABILIZER FWD MOUNT LUG IN CENTER STABILIZER BOX LOWER HOLE HAS CORROSION.SDR Q2SA20160205241Frame · corrodedAFT ACCESSORY BAY BS 1040 FRAME HAS CORROSION ON LOWER FLANGE BETWEEN S27L AND S27R.SDR Q2SA20160126238Door Frame · corrodedAFT CARGO DOOR CUTOUT LOWER AFT CORNER HAS CORROSION.SDR Q2SA20160126237Stringer Clip · corrodedAFT CARGO PIT BS 795, S26R STRINGER CLIP IS CORRODED.SDR Q2SA20160126236Strap · corrodedAFT CARGO BAY BS 759, S25R STRAP HAS CORROSION.
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