Boeing 737-4B7

Service difficulty reports · 5,757

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 = '7374B7'
  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.

SDR USAA040775Pin · corrodedPIT - C3, PIN ASSEMBLIES, 1 INCH BY 1 INCH AREA, CORROSION; NO LEVEL OR TASK. RT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IAW EA 79359/ DRAFT EO 5502V025.Oct 24, 2004 · N448US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA040776Pin · corrodedPIT, C3, PIN ASSEMBLIES- 1INCH X 1INCH AREA, CORROSION; NO LEVEL OR TASK LT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IWA WA 79359/ DRAFT EO 5502V025.Oct 24, 2004 · N448US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA040933Intercostal · corrodedPIT - Q1 - INTERCOSTAL, .75 INCH BY 3 INCHES, CORROSION; LEVEL 1;TASK NR C53-107-02, FRAME 328, LBL 11. CHANGED INTERCOSTAL IAW SRM 51-10-02, 51-20-01, 51-40-01.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040918Frame · corrodedPIT - Q1 - FRAME, 2 INCH BY 1.5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-101-01, FRAME OUTER CHORD BS 227.8, WL 208.1 AND 2 INCH. REMOVED CORROSION, TREATED AND PRIMED, REINSTALLED FASTENERS IAW SRM 51-40-03.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040915Clip · crackedPIT - Q1 - CLIP, .1250 INCH CRACK, STA 807 AND STR 10R. REMOVED AND REPLACED CLIP IAW SRM 51-10-02.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040914Clip · crackedPIT - Q1- CLIP, .2500 INCH CRACK AT STA 807, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040913Clip · crackedPIT - Q1- CLIP, .1250 INCH CRACK AT STA 663.75 AND STR S-10R. REMOVED AND REPLACED CLIP IAW SRM 51-40-03.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040777Skin · crackedPIT - RON, SKIN WITH .5000 INCH CRACK, FWD STA 380 BETWEEN STR 28R AND BL0. INSTALLED DOUBLER IAW EA 79322.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040778Bulkhead · crackedPIT, FPBH INSP, FPBH WEB-.3750 INCH CRACK, STA 178 FWD PRESSURE BULKHEAD LT RADAR ANTENNAE MOUNT. DOUBLER INSTALLED IAW EO 53-V153, JOB CARD MK-4293801.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040779Stiffener · crackedPIT, FPBH INSP, STIFFNER 1 INCH CRACK IN LENGTH, STA 178 UNDER HORIZON STIFFNER WL 218 RT SIDE. DOUBLER INSTALLED IAW EO 5300V153, JOB CARD MK42-93801.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040780Stiffener · crackedPIT, FPBH INSP, STIFFENER TWO CRACKS, .5000 INCH X .7500 INCH LENGTH. STA 178 FPBH WL 218 UNDER HORIZON STIFFENER. DOUBLER INSTALLED IAW EO 5300V153, JOB CARD MK-42-93801.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040923Frame · crackedPIT - Q1 - FRAME, .2500 INCH CRACK, STA 867 BETWEEN STR 8L AND STR 9L. INSTALLED DOUBLER IAW TYP REP 53-10-20A.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040911Stringer Clip · crackedPIT - Q1 - STRINGER TIE CLIP, .2500 INCH CRACK, STA 380, STR 2 LT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040910Stringer Clip · crackedPIT - Q1 - CLIP, .2500 INCH CRACK, RIVET OF STRINGER CLIP, STA 767 S4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040907Tie Clip · crackedPIT - Q1 -CLIP, .1250 INCH CRACK FROM RIVET AT FRAME STA 663.75, STR S10L. REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-10-2, 51-40-03 AND MFG DWG 65-46541.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040909Clip · crackedPIT - Q1 -CLIP, .5 INCH CRACK AT BS578, S8L. DEFECTIVE PART REPLACED WITH IDENT PART IAW IDENT PART IAW SRM 51-40.Oct 20, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040908Clip · crackedPIT - Q1 - CLIP, .5 INCH CRACK, BS 578, S8R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40.Oct 20, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040756Beam · crackedPIT, FPBH, VERTICAL CHORD, .750 INCH LONG, IB RADIUS OF VERTICAL CHORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA 79303.Oct 15, 2004 · N445US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA040774Beam · crackedPIT, FPBH INSP, VERTICAL CORD-.750 INCH LONG CRACK. IB RADIUS OB VERTICAL CORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA79303.Oct 15, 2004 · N445US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA040743Pressure Blkhd · crackedPIT, FPBH, WEB, .1250 INCH CRACK AT RIVET. FWD PRESSURE BULKHEAD, WEB WL 234/RBL 12. WEB REPAIR, FILLER AND DOUBLER IAW SRM 53-10-08, FIG 209 AND EO 5300V153.Oct 11, 2004 · N445US · Boeing 7374B7 · Fuselage Main, BulkheadSDR SB04140Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE FLOOR PATH EMERGENCY LIGHTING AT SEAT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Oct 7, 2004 · N434US · Boeing 7374B7 · Emergency LightingSDR USAA040719Web · gougedCHORD, .7500 INCH X 1.5 INCH X .080 INCH DEEP GOUGE, BS 591 AT RBBL 40 WEB LOWER CHORD RT AIRCO BAY. CUT OUT DAMAGE, INSTALLED FILLER AND STRAPS IAW EA79114.Oct 6, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR SB04138Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS AT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Oct 4, 2004 · N784AU · Boeing 7374B7 · Emergency LightingSDR USAA040831Skin · delaminatedTOP SKIN, CORE BOND, 2 INCH SQUARE AREA, DELAMINATION. LT OB FOREFLAP TOP SKIN SURFACE ON IB T/E. INSTALLED NEW CORE AND TOP DOUBLER, SEAL AND REFINISH IAW SRM.Oct 1, 2004 · N775AU · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040721Angle · corrodedZEE ANGLE, 1 TO 2 INCHES OF CORROSION; 5 PLACES, CORROSION; LEVEL 1; TASK NR C53-107-01, AFT ENTRY DOOR Z ANGLE STA 962-986.Oct 1, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040711Splice · crackedCRACK SPLICE, .5 INCH LONG, STA 908 AND STR 4R, SPLICE. MANUFACTURED NEW SPLICE IAW 51-20-01, 51-20-05.Sep 30, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR SB04131Module · failedCLT - FLT 1021 - AFTER TAKEOFF FROM CLT, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GESep 25, 2004 · N435US · Boeing 7374B7 · Hydraulic System, MainSDR USAA040679Bracket · crackedPIT - FOUND BRACKET CRACKED .5 INCH, FORWARD SERVICE DOOR LOWER AFT CORNER INTERNAL BRACKET. REPLACED BRACKET WITH MANUFACTURED BRACKET PE SRM 52-10-02. (M)Sep 24, 2004 · N436US · Boeing 7374B7 · Service DoorsSDR USAA040617Panel · crackedPIT - FOUND WING PANEL CRACKED 3 INCHES, LEFT ENGINE PYLON, WING UPPER SURFACE FIXED PANEL AFT INBOARD EDGE. INSTALLED DOUBLER AND SEALED PER TYP REPAIR 54-50-14A. (M)Sep 20, 2004 · N434US · Boeing 7374B7 · Wing, Plate/SkinSDR SB04129Relay · unreliableCLT - FLT 1183 - FLIGHT DEPARTED CLT WITH THE NR 1 GENERATOR ON MEL 24-1. ON CLIMB-OUT, EN ROUTE TO MYR, CREW REPORTED, LOST THE LEFT TRANSFER BUSS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT CLT. TRANSFER BUSS CAME BACK Sep 20, 2004 · N440US · Boeing 7374B7 · AC Generation SystemSDR SB04127Battery · dischargedCLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS, AT CABIN SEAT ROWS 12 THROUGH 19, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY ASSEMBLY M1136. OPERATIONAL CHECK GOOD.Sep 19, 2004 · N781AU · Boeing 7374B7 · Emergency LightingSDR USAA040740Angle · corrodedPIT, Q4, Z-ANGLE, 26 INCHES, CORROSION; LEVEL 1; TASK NR C53-107-02, AFT ENTRY DOOR Z-ANGLE AROUND SCREW HOLES, STA 962-986. REPLACED Z-ANGLE, DRILLED HOLES IAW SRM 51-10-02.Sep 17, 2004 · N432US · Boeing 7374B7 · Passenger/Crew DoorsSDR USAA040729Channel · corrodedPIT - Q4, Z-CHANNEL, CORROSION; 1 INCH DIAMETER AREA, LEVEL 1, TASK NR C53-107-01, MED LOWER THRESHOLD, STA 312-344. MANUFACTURED AND INSTALLED NEW Z-CHANNEL IAW DWG 65-17688.Sep 17, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040728Floor Support · separatedPIT - Q4, FLOOR SUPPORT, .1250 INCH GAP, SEPARATION. FLOOR SUPPORT SEPARATED FROM WEB, STA 986.5 BETWEEN STR 17L AND STR 21L. FABRICATED PART TO MATCH ORIGINAL IAW SRM 51-10-02.Sep 17, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040727Web · damagedPIT - Q4, WEB DAMAGED, 11 INCHES LONG, AFT OF STA 986.5 FLOOR LEVEL AFT OF AFT ENTRY DOOR. MANUFACTURED WEB AND INSTALLED IAW SRM 51-10-02 AND DWG NR 65C33533.Sep 17, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040726Crease Beam · corrodedWEB, 1 INCH AREA, CORROSION; NO LEVEL OR TASK, UPPER AND LOWER SURFACE CREASE BEAM, LT SIDE STA 948, 965. MANUFACTURED WEB FROM ALUM MATERIAL IAW SRM 53-60-15.Sep 17, 2004 · N432US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA040725Floor Support · corrodedFLOOR TRACK, ABOUT 3 INCHES LONG BY 1 INCH WIDE AREA, CORROSION; NO LEVEL OR TASK. FLOOR TRACK AT STA 500F + 16 INCHES RBL 17. FABRICATED BY MACHINE SHOP TO MATCH ORIGINAL IAW SRM 53-00-53-202.Sep 17, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040724Floor Support · corrodedFLOOR TRACK, 3 INCHES LONG BY 4 INCHES WIDE, CORROSION; NO LEVEL OR TASK, STA500+ 16 INCHES AT LBL17. FABRICATED AT MACHINE SHOP TO DUPLICATE ORIGINAL IAW SRM 53-00-53, FIG 202.Sep 17, 2004 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040625Attach Angle · corrodedPIT - FOUND ATTACH ANGLE CORRODED THREE AREAS, APPROX 1.5 INCH BY 6 INCHES, STATION 947 FROM RT ZEE ANGLE TO LEFT ZEE ANGLE. MANUFACTURED AND INSTALLED NEW ANGLE PER SRM 51-40-02. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040619Support Angle · crackedPIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, BETWEEN STATION 500 AND 500A MOUNTED TO STRINGER 28L AND 28R. REMOVED AND REPLACED ANGLE PER DWG 65-45783. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040618Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED 6 PLACES, 1 INCH TO 1.5 INCH CRACKS, CENTER LINE OF FLOOR STATION 380-400, TOP OF INTERCOSTAL. FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-02 AND BOEING DWG 69-35365. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040615Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .25 INCH, JUST AFT OF FRAME AT STATION 500B OUTBOARD STRINGER 26R. REPLACED INTERCOSTAL PER SRM 53-00-00. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040623Stringer Clip · crackedPIT - FOUND CLIP CRACKED .5 INCH, STRINGER CLIP, CABIN OVERHEAD BS 601 S6L. INSTALLED NEW CLIP PER SRM 51-40-00. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040622Frame · crackedPIT - FOUND STUB FRAME CRACKED .5 INCH LONG, STATION 360, S11L. FABRICATED NEW CLIP AND INSTALLED PER SRM 51-40-02 AND BOEING DWG 60-48985. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040621Clip · crackedPIT - FOUND CLIP CRACKED .5 INCH, FRAME 847, STRINGER STRINGER S4R. DRILLED NEW CLIP AND REPLACED CLIP PER SRM 53-40-03. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040620Clip · crackedPIT - FOUND ATTACH CLIP CRACKED .5 INCH, FRAME 827, STRINGER S4R. REMOVED OLD TIE CLIP AND INSTALLED NEW ONE PER SRM 53-40-03. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040612Support Angle · crackedPIT - FOUND SUPPORT ANGLE CRACKED 4 INCHES, AFT SIDE OF FRAME AT STATION 500 FORWARD OF VHF ANTENNA CUTOUT. REPLACED ANGLE WITH SAME PART PER SRM 53-10-00 DWG 65-45783. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040611Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH IN LENGTH, INTERCOSTAL MOUNTED TO FRAMES AT 500A AND B, JUST AFT OF 500A. REPLACED INTERCOSTAL PER SRM 53-10-02. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040614Skin · crackedPIT - FOUND PYLON CUT OUT CRACKED APPROX 1 INCH, NR 2 ENGINE PYLON ACCESS PANEL NR 5827R AFT INBOARD CORNER. INSTALLED DOUBLER PER TYP REPAIR 54-30-07. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Wing, Plate/SkinSDR USAA040613Support · crackedPIT - FOUND ANTENNTA SUPPORT CRACKED .5 INCH BY .25 INCH CRACK TWO PLACES, BETWEEN STATION 500A AND 500B BL0, VHF CUTOUT STRUCTURE. MFG CHANNEL, ALODINED, PRIMED PER DWG 65-45783 SRM 53-10-00. (M)Sep 17, 2004 · N434US · Boeing 7374B7 · Fuselage Miscellaneous Structure
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