Boeing 737-3B7

Service difficulty reports · 4,722

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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 = '7373B7'
  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 USAA002114Fitting · corrodedPIT - FOUND CLEVIS LUG CORRODED .007 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION BOTTOM AFT CLEVIS BONE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUG WITHIN THE LIMITS IN SRM 55-10-10. OVERSIZE MANUFACTURED. (M)Oct 24, 2000 · N518AU · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA002115Clevis · corrodedPIT - FOUND CLEVIS LUG CORRODED .014 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION BOTTOM FORWARD CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUGS WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUFACTURED. (M)Oct 24, 2000 · N518AU · Boeing 7373B7 · Empennage Flight Control Surfaces, Attach FittingsSDR USAA002116Clevis · corrodedPIT - FOUND CLEVIS LUG CORRODED .018 DEEPEST AREA, RIGHT HORIZONTAL STAB CENTER SECTION TOP FORWARD CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUGS WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUF. (M)Oct 24, 2000 · N518AU · Boeing 7373B7 · Empennage Flight Control Surfaces, Attach FittingsSDR USAA002117Clevis · corrodedPIT - FOUND CLEVIS LUG CORRODED .004 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION TOP AFT CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUG WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUFACTURE. (M)Oct 24, 2000 · N518AU · Boeing 7373B7 · Empennage Flight Control Surfaces, Attach FittingsSDR AWXA0000791Light · inoperativeNON ROUTINE LINE, RT OVERWING EMERGENCY PATHWAY LIGHTING INOP. REMOVED AND REPLACED FLOOR MOUNTED LIGHT MODULE, OPS CHECK GOOD.Oct 23, 2000 · N332AW · Boeing 7373B7 · Emergency LightingSDR USAASB00299Pump · leakingATL-CLT - FLT 1273 - DURING APPROACH, THE A-HYDRAULIC QUANTITY DROPPED TO THE STAND PIPE LEVEL AND THE LOW PRESSURE LIGHT ILLUMINATED. MAINTENANCE REPLACE THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. THE ENGINE DRIVEN CASE DRAIN AND PRESSURE FILTERS WERE REPLACED.Oct 22, 2000 · N517AU · Boeing 7373B7 · Hydraulic Pump (Electric/Engine), MainSDR USAASB00297Light · failedROA-PIT - FLT 1295 - AFTER LANDING GEAR EXTENSION THE RIGHT MAIN GEAR DOWN LOCK LIGHT DID NOT ILLUMINATE. A VISUAL INSPECTI0N COULD NOT CONFIRM THE LANDING GEAR WAS DOWN AND LOCKED. THE GEAR WAS EXTENDED MANUALLY BUT THERE WAS STILL NO DOWN AND LOCKED INDICAOct 21, 2000 · N510AU · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA001786Skin · crackedCLT - FOUND NR 3 SLAT SKIN CRACKED .25 INCH, LOWER SKIN AFT FASTENER ROW 4 INCHES L/B ACTUATOR. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Oct 19, 2000 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA001785Skin · crackedCLT - FOUND SKIN AND DOUBLER CRACKED 1 INCH, NR 1 PYLON AT ACCESS PANEL 5728L. INSTALLED DOUBLER PER TR 54-30-07. (M)Oct 19, 2000 · N516AU · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA001774Door Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, LEFT AFT DOOR FRAME UPPER HINGE FITTING. REPLACED FITTING PER SRM 51-10-02. (M)Oct 18, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAASB00295Switch · damagedPIT - FLT 1140 - EN ROUTE FROM LGA-PIT, FLIGHT LOST PRESSURIZATION AT FL220. DESCENDED TO FL090 AND SET PRESSURIZATION SYSTEM MANUAL. OXYGEN MASKS DEPLOYED NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT PIT. MAINTENANCE FOUND A DAMAGED COMPRESSOR DISCOct 16, 2000 · N514AU · Boeing 7373B7 · Cabin Cooling SystemSDR DL733002037Fitting · crackedINSPECTION OF THE RT WING MLG BEAM OUTBOARD ATTACH FITTING REVEALED A CRACK EMANATING FROM A FASTENER HOLE COMMON TO THE REAR SPAR UPPER CHORD. INSPECTION OF THE BOLT HOLE REVEALED TOOLING DAMAGE COMMON TO THE REAR SPAR CAP AND WEB. THE HOLE WAS OVERSIZED TOOct 16, 2000 · N951WP · Boeing 7373B7 · Wing, Landing Gear Attach FittingsSDR DL733002036Fitting · crackedTHE MLG BEAM OUTBOARD AFT ATTACH FITTING WAS FOUND WITH A TYPICAL CRACK EMANATING FROM AN ATTACHMENT HOLE COMMON TO THE REAR SPAR UPPER CHORD. BOLT HOLE HFEC INSPECTION REVEALED A CRACK IN THE SPAR WEB AT THE FASTENER LOCATION. THE HOLE WAS OVERSIZED TO REMOOct 16, 2000 · N951WP · Boeing 7373B7 · Wing, Attach FittingsSDR USAA001733Frame · crackedTPA - CX-5, FRAME CRACKED, 6 INCHES, AFT CARGO DOOR FORWARD LOWER CORNER FRAME. REPLACED FRAME PER SRM 51-10-1. (X)Oct 12, 2000 · N387US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001731Stringer · crackedCLT - Q-4, STRINGER CRACKED, 2 INCHES, LEFT SIDE STR 5A, AFT STA 1138 FRAME. REPAIRED ANGLES AND DOUBLER PER SRM 53-00-01. (X)Oct 12, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA001722Bulkhead · crackedCLT - Q-4, SKIN CRACKED, STA 178, RBL 7, WL 210.5. INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08 FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001721Bulkhead · crackedCLT - Q-4, BULKHEAD CRACKED, .25 INCH, BS 178, WL 206.5, RBL 1.0. INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08 FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001720Bulkhead · crackedCLT - Q-4, WEB CRACKED, .25 INCH, STA 178, RBL 1, WL 206. INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08 FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001719Bulkhead · crackedCLT - Q-4, BULKHEAD CRACKED, .50 INCH, BS 178, WL 202, RBL 5.5. INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001718Bulkhead · crackedCLT - Q-4, BULKHEAD CRACKED, 1 INCH, BS 178, WL 202, LBL 5.5. INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08 FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001717Bulkhead · crackedCLT - Q-4, BULKHEAD CRACKED, .25 INCH, BS 178, WL 199, LBL 5.5. REMOVED AND INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08, FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001716Bulkhead · crackedCLT - Q-4, SKIN CRACKED, 1 INCH, BS 178, WL 195, RBL 5.7. REMOVED AND INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08 FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001715Bulkhead · crackedCLT - Q-4, SKIN CRACKED, 1 INCH, BS 178, WL 195, LBL 5.7. REMOVED AND INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08, FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001714Bulkhead · crackedCLT - Q-4, SKIN CRACKED, 1 INCH, RBL 5, WL 188, STA 178. REMOVED CRACK, INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08, FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001713Bulkhead · crackedCLT - Q-4, BULKHEAD CRACKED, .50 INCH, BS 178, WL 188, RBL 1.0. INSTALLED DOUBLER PER EA 68148 AND SRM 53-10-08 FIG 203. (X)Oct 10, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAASB00288Heat Exchanger · defectiveSDF - FLT 985 - EN ROUTE FROM DCA TO MCI, AT FL310, THE NR 1 ENGINE HIGH OIL TEMPERATURE WENT INTO THE YELLOW BAND. CAPTAIN REDUCED POWER AND THE GAUGE WENT BACK TO NORMAL. FLIGHT DIVERTED TO SDF AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED AND NOOct 5, 2000 · N526AU · Boeing 7373B7 · Engine Oil CoolerSDR USAA002109Bracket · crackedPIT - FOUND ANGLE BRACKET CRACKED .25 INCH, STATION 380 BETWEEN STRINGER 8 AND 9 RT OVERHEAD BIN ATTACH PT. INSTALLED .045 INCH ANGLE DOUBLER PER US AIRWAYS TYPICAL REPAIR 53-10-14. (M)Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002111Web · crackedPIT - FOUND WEB CRACKED 1.5 INCH, WL 207, RBL 28 AFT STATION 178 LIGHTENING HOLE. REMOVED, FABRICATED NEW WEB FROM .071 2024-T3 AND INSTALLED. (M)Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001674Stiffener · crackedCLT - Q-4, VERTICAL STIFFENER CRACKED .5 INCH AFT SIDE BULKHEAD 178, WL 184, LBL 5.7 ON INBOARD SIDE. INSTALLED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001673Skin · crackedCLT - Q-4, SKIN CRACKED .50 INCH AT RIGHT AFT CORNER ACCESS PANEL AT NAC STA 225. INSTALLED FILLER AND DOUBLER PER TR 54-30-07. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA001726Skin · crackedPIT - SKIN CRACKED .25 INCH, STA 440 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED .045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X)Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001725Skin · crackedPIT - SKIN CRACKED .25 INCH, STA 380 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED .045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X)Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001724Bulkhead · crackedPIT - SKIN CRACKED 1.5 INCHES, WL 207, RBL 28 AFT STA 178 LIGHTENING HOLE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER; REMOVED, FABRICATED NEW WEB FROM .071 INCH 2024-T3 AND INSTALLED. (X)Oct 3, 2000 · N376US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001672Floorbeam · corrodedCLT - Q-4, T-CAP/FLOORBEAM CORRODED, 2 INCHES BY 100 INCHES, CORROSION LEVEL 1, STA 328. REPLACED T-CAP PER SRM 53-10-52, FIG 205. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001671Seat Track · corrodedCLT - Q-4, SEAT TRACK CORRODED, 24 INCHES, CORROSION LEVEL 1 C53-107-02, CENTER BETWEEN STA 328 AND STA 344. REPLACED SEAT TRACK PER SRM 53-00-92. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA001670Floorbeam · corrodedCLT - Q-4, FLOORBEAM CORRODED, .50 INCH X 2 INCH, CORROSION LEVEL 1 C53-107-02, STA 294.5, BL ZERO TO RBL 52. SPLICED T-CAP PER SRM 53-10-51. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001669Floorbeam · corrodedCLT - Q-4, FLOORBEAM CORRODED, 2 INCH BY 1 INCH, STA 312, LBL 50 TO RBL 50. CORROSION LEVEL 1 C53-107-02. REPAIRED PER SRM 53-10-51. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001668Floorbeam · corrodedCLT - Q-4, FLOORBEAM CORRODED, 120 INCHES, CORROSION LEVEL 1, STA 986.5 T-CAP AREA. INSTALLED NEW T-CAP AND DOUBLER PER TR 53-60-01. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001667Floorbeam · corrodedCLT - Q-4, FLOORBEAM CORRODED, 120 INCHES, CORROSION LEVEL 1. STA 967 T-CAP AREA OF FLOORBEAM. INSTALLED NEW T-CAP AND DOUBLER PER TR 53-60-01. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001666Floorbeam · corrodedCLT - Q-4, FLOORBEAM CORRODED, 2 INCHES BY 2 INCHES, CORROSION LEVEL 1 AT FLOORBEAM STA 967, BL 31. INSTALLED NEW T-CAP AND DOUBLER PER TR 53-60-01. (X)Oct 3, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAASB00280Uplock Switch · failedGSO - FLT 1658 - ON CLIMB-OUT, AFTER GEAR RETRACTION, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CREW RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO FIELD AT GSO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENOct 1, 2000 · N393US · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA001644Beam · corrodedCLT - FOUND CREASE BEAM WEB CORRODED 1 INCH BY 2 INCHES IN 6 PLACES, BETWEEN STATION 847-867 STRINGER 17L. CORROSION LEVEL 1, TASK NR C53-107-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-2. (M)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001643Web · corrodedCLT - FOUND WEB CORRODED 5 INCHES BY 1.5 INCHES, STRINGER 17L BETWEEN STATION 847-867. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED WEB PER SRM 51-10-02. (M)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001646Angle · corrodedCLT - FOUND SURFACE CORROSION ON Z-ANGLE, 45 INCHES LONG, STATION 955-994 RBL 54. CORROSION LEVEL 1, TASK NR C53-107-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02 AND 51-20-01. (M)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001645Angle · corrodedCLT - FOUND SURFACE CORROSION ON Z-ANGLE, 41 INCHES LONG, STATION 950 TO 994 RBL 55. CORROSION LEVEL 1, TASK NR C53-107-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-20-01 AND 51-10-02. (M)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001642Stringer Clip · crackedCLT - FOUND TIE BRACE CRACKED .250 INCH, STATION 294.5 STRINGER 17R. REPLACED TIE CLIP PER SRM 51-10-2. (M)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001647Crease Beam · corrodedCLT - Q-4, CREASE BEAM 20 SQUARE INCHES OF CORROSION. CORROSION LEVEL 1, TASK NR C53-107-01. S17R CREASE BEAM STA 616 - STA 639. REMOVED OLD CREASE BEAM WEB AND REPLACED WITH NEW PART PER SRM 53-60-13. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA001641Tie Clip · crackedCLT - Q-4, TIE CLIP HAD .1250 INCH CRACK AT STA 500A STR 2L. REPLACED TIE CLIP PER SRM 51-10-2. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001640Frame · crackedCLT - Q-4, FRAME HAD .25 INCH CRACK AT STA 887 S8R - S 9R. FABRICATED DOUBLER AND INSTALLED PER TR 53-10-14. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001639Frame · crackedCLT - Q-4, FRAME HAD .1250 INCH CRACK AT STA 480 STR 9R. FABRICATED DOUBLER, HEAT TREATED AND INSTALLED PER TR 53-10-14. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Frame
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