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 USAA070345Support · crackedSTA 727D + 12 INCHES AT RBL 2, ANTENNA BRACKET SUPPORT MOUNT CRACKED. DRILLED & INSTALLED NEW PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH.May 1, 2007 · N430US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA070354Tie Clip · crackedSTA 807 STR 4, STRINGER TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .5 INCH.May 1, 2007 · N430US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA070343Frame · crackedSTUB FRAME ATTACH POINT BS 616 & LBL 64 CRACKED. INSTALLED REPAIR ANGLE PER TYP REP 53-62-05, DEFECT SIZE: .250 INCH.May 1, 2007 · N430US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA070341Frame · crackedSTA 500C BETWEEN STR 8 & 9, RT AT ATTACH BRACKET AT INBD RIVET HOLE. INSTALLED REPAIR ANGLES PER TR 53-10-20E. DEFECT SIZE: 1/4"May 1, 2007 · N430US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA070340Frame · crackedSTA 480 BETWEEN STR 8 & 9 RT AT ATTACH BRACKET ON FRAME, INBD RIVET. INSTALLED REPAIR ANGLES PER TR 53-10-20E. DEFECT SIZE: 1/4"May 1, 2007 · N430US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA070339Floor Support · crackedBETWEEN BL0 TO LBL -24 AT STA 540. REMOVED & REPLACED SUPPORT ANGLE PER SRM 51-10-02. DEFECT SIZE: 1"May 1, 2007 · N430US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA070344Mount · crackedSTA 727D+12 AT RBL 2, ANTENNA MOUNT Z SUPPORT. DRILLED & INSTALLED NEW PART PER SRM 51-10-02. DEFECT SIZE: 1 INCHMay 1, 2007 · N430US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA200705002Skin · cracked2" CRACK FOUND AT RT HORIZ STAB LOWER SKIN CENTER OF 3" PANEL. (CLT) INSTALLED TEMPORARY DOUBLER PER TR 55-10-07 REV B.Apr 29, 2007 · N438US · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAA200705001Skin · cracked1" CRACK FOUND AT STA 727D STR 23L ON SKIN. (CLT) INSTALLED DOUBLER PER TR 53-60-03AApr 29, 2007 · N438US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR SB07035Iru · failedMCO FLT 1672 - CLIMBING THROUGH 3,000 FEET OUT OF MCO, EN ROUTE TO BWI, CREW REPORTED BOTH ADI'S AND HSI'S FAILED. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 IRU.Apr 28, 2007 · N458UW · Boeing 7374B7 · Inertial Guidance SystemSDR USAA200704004Skin · cracked1.5" CRACK FOUND AT L2 DOOR LOWER HINGE CUT OUT. INSTALLED DOUBLER/TRIPLER PER EA 84451.Apr 22, 2007 · N450UW · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR SB07030Battery Pack · dischargedCLT - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M01132. OPERATIONAL CHECK GOOD.Apr 18, 2007 · N432US · Boeing 7374B7 · Emergency LightingSDR SB07029Module · faultyIAD FLT1724, ON DESCENT, CREW REPORTED THERE WAS NO INDICATION OF GEAR EXTENSION (RED OR GREEN LIGHTS) WHEN LANDING GEAR HANDLE WAS PUT IN THE DOWN POSITION. CREW PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES AND EXTENDED THE GEAR MANUALLY. STILL NO LIGHTS. FLApr 17, 2007 · N434US · Boeing 7374B7 · Flight Compartment LightingSDR SB07028Charger · inoperativeDCA - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.Apr 17, 2007 · N440US · Boeing 7374B7 · Emergency LightingSDR USAA200704002Skin · cracked1.25 INCH CRACK FOUND ON SKIN AT STA 944 AND S-24L. REPAIR: INSTALLED DOUBLER IAW EA 98606.Apr 10, 2007 · N457UW · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA200704003Skin · cracked2.5 INCH CRACK FOUND AT LOWER SKIN AT STAB ST. 98-100 (TE). INSTALLED DOUBLER IAW EA 98607 AND TR 55-10-07B.Apr 10, 2007 · N457UW · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAA200704001Skin · crackedA 3 INCH CRACK FOUND ON SKIN, RIGHT SIDE AT STA 727E + 3 INCHES. REMOVED DAMAGED AREA & INSTALLED REPAIR DOUBLER PER SRM 53-00-01 REP 31.Apr 4, 2007 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR SB07024Battery Pack · dischargedBDL - MAINTENANCE REPORTED THE FORWARD LEFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Mar 28, 2007 · N459UW · Boeing 7374B7 · Emergency LightingSDR USAA200703005Skin · crackedA .75 INCH CRACK FOUND AT LEFT PYLON AT ACCESS PANEL 5727L OPENING. STOP DRILLED & INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07.Mar 27, 2007 · N426US · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA070227Frame · crackedBS 492 S-24R HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98545, DEFECT SIZE: .5 INCH.Mar 20, 2007 · N445US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA070228Skin · puncturedRIGHT AILERON, UPPER SURFACE, 10.5 INCHES INBOARD OF OUTBOARD EDGE PUNCTURED. REMOVED DAMAGE, LAYED UP PLIES PER EA 98560, DEFECT SIZE: .5 INCH.Mar 20, 2007 · N452UW · Boeing 7374B7 · AileronsSDR USAA070222Frame · crackedSTA 440 STR 24R O/B RADIUS OF FRAME CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98545, DEFECT SIZE: 1 INCH.Mar 19, 2007 · N445US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA200703001Skin · crackedA 2.25 INCH CRACK FOUND AT LT HORIZONTAL STAB LWR SKIN STA 115. INSTALLED DOUBLER PER SRM 55-10-01.Mar 12, 2007 · N441US · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR SB07019Battery Pack · dischargedPHL MAINTENANCE REPORTED THE FORWARD SERVICE DOOR LOWER EMERGENCY EXIT SIGN ALONG WITH THE ONE ABOVE THE DOOR WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Feb 26, 2007 · N440US · Boeing 7374B7 · Emergency LightingSDR SB07018Battery Pack · dischargedPIT MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT FOR THE LEFT FORWARD OVERWING EMERGENCY ESCAPE DOOR, BETWEEN SEAT ROWS 10 AND 11, WAS INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD.Feb 23, 2007 · N449US · Boeing 7374B7 · Emergency LightingSDR USAA200702001Rib · crackedCRACK FOUND AT RIB 135.5 SKIN CLIP CRACKED BETWEEN STR 2 & 3. REPAIRED PER EA 84116.Feb 23, 2007 · N24893 · Boeing 7374B7 · Wing, Rib/BulkheadSDR SB07017Battery Pack · dischargedDCA - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-00. OPERATIONAL CHECK GOOD.Feb 22, 2007 · N451UW · Boeing 7374B7 · Emergency LightingSDR SB07016Flap · out of rigCLT FLT750 ON DESCENT INTO CLT FROM GCM, WHEN FLAPS WERE SELECTED TO 30 UNITS, THE AIRCRAFT ROLLS TO THE LEFT. WINGS CAN BE KEPT LEVEL WITH 3 DEGREES OF RIGHT AILERON. FUEL WAS BALANCED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE CABLE DFeb 21, 2007 · N459UW · Boeing 7374B7 · Trailing Edge Flap Control SystemSDR USAA070108Door Frame · crackedFWD CARGO DOOR, AFT FUSELAGE FRAME, O/B OF UPPER I/B STOP BOLT HOLE CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98497, DEFECT SIZE: .075 INCH.Feb 20, 2007 · N439US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA070109Door Frame · crackedSTA 440 S-21R CARGO DOOR FUSELAGE FRAME, UPPER I/B STOP BOLT HOLE CRACKED. REMOVED DAMAGE & INSTALLED PARTS PER EA 98496, DEFECT SIZE: .5 INCHES.Feb 20, 2007 · N439US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA070110Door Frame · crackedRADIATING FROM UPPER I/B STOP BOLT HOLE, STA 492.4, S-24R, FWD CARGO DOOR CRACKED. INSTALLED DOUBLER PER EA 98497, DEFECT SIZE: .5 INCHES.Feb 20, 2007 · N439US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA070111Door Frame · damagedRADIATING FROM LOWER O/B STOP BOLT HOLE, STA 492.4, S24R, FWD CARGO DOOR DAMAGE. INSTALLED DOUBLER PER EA 98497, DEFECT SIZE: .375 INCH.Feb 20, 2007 · N439US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA070105Frame · crackedBS 440 S-24R WL 160 CRACKED. TRIMMED OUT CRACK, HEAT TREATED, INSTALLED REPAIR DOUBLERS PER EA 98453, DEFECT SIZE: 1 INCH.Feb 14, 2007 · N440US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA070106Frame · crackedBS 492, S-24R, WL 160 CRACKED. REPLACED FRAME PER DWG 65-20723, DEFECT SIZE: .5 INCH.Feb 14, 2007 · N440US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA070094Skin · crackedLT ENG PYLON PANEL OPENING 5727L AT O/B AFT CORNER OF OPENING. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5".Feb 13, 2007 · N440US · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR SB07012Hydraulic Line · leakingCLT FLT1786 EN ROUTE FROM JAX TO CLT, DURING CRUISE, CREW REPORTED LOSS OF B-HYDRAULIC SYSTEM AS HYDRAULIC QUANTITY RAPIDLY WENT DOWN TO 1/4. THE FIRST INDICATION WAS NR 2 ENGINE BELOW PRESSURE LIGHT, FOLLOWED BY LOSS OF B-HYDRAULIC FLUID AND THEN B-SYSTEM LOFeb 11, 2007 · N444US · Boeing 7374B7 · Hydraulic System, MainSDR USAA070090Angle · crackedBS 348 S-15L CRACKED. REPLACED WITH IDENTICAL PART PER BOEING DWG 64-17685-37, DEFECT SIZE: .250 INCH.Feb 9, 2007 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAASB07011Indicator · faultyBDL FLT 1067 - AFTER TAKEOFF AND FLAP SELECTION TO 1, CREW REPORTED A FLAP ASYMMETRY LOCKOUT. POINTERS ON FLAP POSITION INDICATOR WERE LEFT AT 2 AND RIGHT AT 5. AIRCRAFT CIRCLED BDL TO BURN OFF FUEL TO AVOID AN OVERWEIGHT LANDING. FLIGHT RETURNED TO FIELD AFeb 8, 2007 · N456UW · Boeing 7374B7 · Trailing Flap Position Indicating SystemSDR USAA070082Angle · crackedINTERCOSTAL ANGLE STA 360 AND S-8L CRACKED. MANUFACTURED PART PER DWG 69-48985, DEFECT SIZE: .75 INCH.Feb 6, 2007 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA070083Angle · crackedBS 360 S-13L CRACKED. REMOVED & REPLACED WITH FABRICATED PART PER BOEING DWG 65-17685, DEFECT SIZE: .250 INCH.Feb 6, 2007 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA070084Intercostal · crackedSTA 360 & S-11L CRACKED. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER BOEING DWG 65-17685, DEFECT SIZE: 1 INCH.Feb 6, 2007 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA070085Skin · crackedLEFT ENGINE PYLON PANEL OPENING 572L AT O/B AFT CORNER OF OPENING CRACKED. STOP DRILLED CRACK & INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5 INCH.Feb 6, 2007 · N440US · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA070080Skin · chafedOUTBOARD END OF LEFT WING OUTBOARD MID FLAP CHAFED. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-53-03, DEFECT SIZE: 1 X 2 INCHES.Feb 5, 2007 · N460UW · Boeing 7374B7 · Trailing Edge FlapsSDR USAASB07010Speed Switch · faultyCLT FLT 1081 FLIGHT DEPARTED PIT EN ROUTE TO FLL WITH THE NR 2 GENERATOR/CSD INOPERATIVE. DURING CRUISE, AT FL340, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU AUTO SHUTDOWN. WITH ONLY ONE GENERATOR REMAINING, CREW DIVERTED FLIGHT TO CLT WITHOUT INCIDENT.Jan 30, 2007 · N444US · Boeing 7374B7 · APU ControlsSDR SB07007Windshield · crackedDCA FLT 1781 EN ROUTE FROM MHT TO DCA, THE FIRST OFFICER'S WINDSHIELD ARCED, THEN CRACKED. APPEARS TO BE THE OUTER PANE THAT CRACKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT DCA. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S WINDSHIELD PER MM 56-11Jan 25, 2007 · N449US · Boeing 7374B7 · Flight Compartment WindowsSDR USAA070059Skin · crackedE&E AREA EXHAUST PORT FOR EQUIPMENT COOLING HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98416, DEFECT SIZE: 1 INCH.Jan 24, 2007 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA070060Skin · crackedBS 379 BL 0 HAS CRACK. REMOVED DAMAGE, INSTALLED REPAIR PARTS, INSTALLED DOUBLER PER EA 98415, DEFECT SIZE: 1 INCH.Jan 24, 2007 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA070061Door Frame · crackedFWD CARGO DOOR/FWD FRAME AT 1F FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER EA 98414, DEFECT SIZE: 2 INCHES.Jan 24, 2007 · N442US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA070062Door Frame · crackedFWD CARGO/AFT DOOR FRAME AT 1A STOP FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER & TRIPLER PER EA 98413, DEFECT SIZE: .100 INCH.Jan 24, 2007 · N442US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA070063Door Frame · crackedFWD CARGO DOOR/FWD FRAME AT 1F FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS FROM EA 98414, DEFECT SIZE: 2 INCHES.Jan 24, 2007 · N442US · Boeing 7374B7 · Fuselage Main, Structure
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