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 USAA050205Clip · crackedPIT - FOUND FRAME CLIP CRACKED .5 INCH, STATION 706 S11L. FABRICATED AND INSTALLED NEW CLIP PER SRM 51-46-03 AND 51-70-11. (M)Jan 1, 2005 · N436US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050190Tie Clip · crackedPIT - FOUND STRINGER TIE CLIP CRACKED, .5 INCH IN RADIUS AREA, STRINGER TIE CLIP, STATION 1006, STRINGER 2R. DEFECTIVE PART REPLACED WITH IDENT PART PER TYPICAL REPAIR 57-50-55. (M)Jan 1, 2005 · N436US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050025Structure · crackedPIT - FOUND FWD SERVICE DOOR CRACKED 1.25 INCHES, LOWER A/C STOP FITTING INNER DOUBLER AT FASTENER. MANUFACTURED NEW DOULER AND INSTALLED PER BOEING DWG 6969854. (M)Jan 1, 2005 · N443US · Boeing 7374B7 · Service DoorsSDR USAA050059Door Frame · corrodedPIT - FOUND FRAME CORRODED 1 INCH IN DIAMETER, STATION 492.4, FORWARD CARGO DOOR FRAME AFT LOWER STOP FITTING. CUT OUT DAMAGE, TRIMMED ANGLE TO SIZE AND SHAPE, FABRICATED FILLER, TREATED, PRIMED PER SRM 51-70-11. (M)Jan 1, 2005 · N443US · Boeing 7374B7 · Fuselage Main, StructureSDR SB04170Odor · detectedJAX - FLT783 - JUST AFTER TAKEOFF FROM PHL, EN ROUTE TO JAX, CREW REPORTED A BURNING RUBBER ODOR IN THE COCKPIT THAT LASTED FOR 10 TO 15 SECONDS. CREW SUSPECTED A TIRE PROBLEM BUT NO ABNORMAL LANDING GEAR OR ENGINE INDICATIONS WERE NOTED. TOWER IN PHL REQUESDec 22, 2004 · N437US · Boeing 7374B7 · Air Distribution SystemSDR SB04165Reflector · failedPIT - MAINTENANCE REPORTED THE AFT SERVICE DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR ASSEMBLY. OPERATIONAL CHECK GOOD.Dec 12, 2004 · N430US · Boeing 7374B7 · Emergency LightingSDR SB04163Charger · failedPHL - MAINTENANCE REPORTED THE RIGHT EMERGENCY EXIT HATCH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK AT STA 598R. OPERATIONAL CHECK GOOD.Dec 9, 2004 · N781AU · Boeing 7374B7 · Emergency LightingSDR USAA040939Frame · crackedPIT - Q1 -FRAME, 1 INCH CRACK, RT STA 601 BELOW S17R, FRAME TO FLOORBEAM ATTACH POINT. INSTALLLED REPAIR ANGLE IAW EA 79352.Nov 19, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040970Fitting · crackedPIT - Q1 - FITTING, .25 INC CRACK, RT MLG SUPPORT FITTING, NR 2 HOLE; MODIFIED PART INSTALLED, REPLACED IAW EO 5702V054.Nov 18, 2004 · N435US · Boeing 7374B7 · Wing, Landing Gear Attach FittingsSDR SB04155Charger · inoperativeMAINTENANCE REPORTED AN EMERGENCY LIGHT IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.Nov 17, 2004 · N777AU · Boeing 7374B7 · Emergency LightingSDR USAA041042Skin · delaminatedPIT - Q1 - UPPER AND LOWER SKIN, 3.5 INCH X 2 INCH AREA, DELAMINATION, LT IB AFT FLAP OB END UPPER AND LOWER SURFACE. REMOVED DISBONDED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP SKIN DOUBLER IAW SRM.Nov 15, 2004 · N435US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040930Gusset · crackedPIT - Q1 - GUSSET, .7500 INCH CRACK, BS 927 UNDER RT IB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Nov 12, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040929Frame · crackedPIT - Q1 - FRAME, .2500 INCH CRACK, FRAME 727F BETWEEN S8L AND S9L. CUT OUT CRACKED SECTION AND INSTALLED REPAIR ANGLES IAW TYP REP 53-10-20A AND EA 79502.Nov 11, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040867Skin · crackedSKIN, 1.5 INCH CRACK, STA 727D AT STR 23 RT. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01.Nov 11, 2004 · N439US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040938Skin · damagedPIT - Q1- SKIN, 2 INCH BY 2 INCH AREA, CARBON FIBER DAMAGE, 120.5 INCH UP FROM BOTTOM, 6.25 INCH FORWARD OF T/E. FILLED AND INSTALLED REPAIR PLIES IAW 51-70-17 AND EA 79467.Nov 10, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA040936Skin · wornPIT - Q1 - SKIN, 1 INCH BY 1.5 INCHES WEAR, KNIFE EDGE WEAR, 1 INCH AFT OF FWD CORNER AT RUDDER STA. INSTALLED REPAIR PLIES IAW EA 79467, SRM 51-70-17.Nov 10, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041051Skin · corrodedPIT - Q1 -RUDDER TOP LAYER, .1250 INCH X .1250 INCH X .005 INCH DEEP PIT, 8.25 INCH FWD OF T/E, 72 INCHES DOWN FROM TIP. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041050Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .3750 INCH X .1875 INCH AREA, DELAMINATION, 3 INCH AFT OF NR 6 HINGE CUTOUT. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041048Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION, 32 INCHES FWD OF T/E, 54.5 INCH UP FROM BOTTOM LT SIDE. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTILAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041047Skin · damagedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DAMAGE, 37 INCH FWD OF T/E, 48 INCH UP FROM BOTTOM. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI-LAYERED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041046Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 1 INCH AREA DAMAGE, RUDDER LT SIDE 95.5 INCHES FROM BOTTOM AND 20 INCHES FWD OF T/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041045Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA, SINGLE LAYER DAMAGE. RUDDER LT SIDE 105./5 INCHES FROM BOTTOM AND .3750 FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI PLY REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041044Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA OF DAMAGE, RUDDER LT SIDE 98.5 INCH FROM BOTTOM AND 9.25 INCHES FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041041Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION 28 INCH FWD OF T/E, 39 INCH UP FROM BOTTOM. PREPARED DAMAGED AIR, INSTALLED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR SB04153Charger · inoperativeCLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 15 THROUGH 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.Nov 7, 2004 · N432US · Boeing 7374B7 · Emergency LightingSDR USAA040937Skin · delaminatedPIT - Q1 - SLAT 15 INCH BY 6 INCH DELAMINATION. NR 3 SLAT IB END. REMOVED TOP SKIN AND CORE, INSTALLED INTERNAL DOUBLER, CORE, TOP SKIN TYP REP 57-42-03, SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7 · Leading Edge DevicesSDR USAA040935Skin · delaminatedPIT - Q1 - FLAP, 4.5 INCHES BY 5 INCHES DELAMINATION, IB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040934Skin · delaminatedPIT - Q1 - FLAP, 3.5 INCH BY 5 INCH AREA, DELAMINATED, OB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040919Angle · crackedPIT - Q1 - T-ANGLE, 3 INCH BY 4 INCH AREA CRACKED AND PULLED. OUTBD SLING ATTACH POINT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Nov 5, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040841Skin · delaminatedSKIN, 4 INCH BY 14 INCH AREA DELAMINATION, LT OB FOREFLAP T/E IB END. DEFECTIVE PART REPLACED WITH IDENT PN.Nov 5, 2004 · N776AU · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040920Skin · incorrectPIT - Q1- SKIN, 12 INCH BY 6 INCH INCORRECT DOUBLER REPAIR, FRAME ST 344 S19R. OLD DOUBLER REMOVED AND NEW DOUBLER INSTALLED TO COMPLY WITH NEW SRM DIRECTIONS IAW SRM 53-00-01, FIG 231.Nov 4, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040840Bulkhead · crackedC3, BULKHEAD WEB, 3 CRACKS, .1250 INCH, FPBH BS 178, RBL 6, WL 210 AND 213. DOUBLER INSTALLED IAW EO 5300V153.Nov 4, 2004 · N776AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040932Angle · corrodedPIT - Q1 - ZEE ANGLE, 2 INCH BY 3 INCH AREA, CORROSION LEVEL 1, TASK NR C53-100-1, BS 796, S25R IN AFT CARGO BIN. REMOVED ZEE ANGLE, AND INSTALLED NEW IAW SRM 51-10-2.Nov 3, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040924Track · crackedPIT - Q1 - TIE DOWN TRACK, CORROSION AND CRACK, 2 INCH BY 4 INCH AREA AND 1 INCH CRACK. CORROSION; LEVEL 1: TASK NR C 53-208-01, BS 727F, S 26L. CUT OUT DAMAGED SECTION AND SPLICED IN NEW IAW SRM 53-00-53, FIG 202.Nov 3, 2004 · N435US · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040839Bulkhead · crackedPIT - C3, SKIN, 2 CRACKS, 1 INCH IN LENGTH TOTAL, FPBH WL 234, BL7R. DOUBLER REPAIR IAW SRM 53-10-08, FIG 209.Nov 3, 2004 · N776AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA041043Skin · delaminatedPIT - Q1 - TOP SKIN, 3 INCH X 3 INCH AREA AND LOWER SKIN DAMAGE 1 INCH SQUARE, DELAMINATION AND SKIN DAMAGE, NR 4 SLAT TOP SURFACE T/E. INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER IAW SRM.Nov 2, 2004 · N435US · Boeing 7374B7 · Leading Edge DevicesSDR USAA040926Frame · crackedPIT - Q1 - FRAME, .1250 INCH CRACK, BS787 AT S9L-S8L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR ANGLES IAW TYP REP 53-10-02A.Nov 2, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040925Seat Track · crackedPIT - Q1 - SEAT TRACK, .75 INCH LONG CRACK, IB RT SEAT TRACK STA 727B, UPPER FLANGE LOWER SURFACE AT VERTICAL RADIUS. CUT OUT SECTION AND REPLACED NEW AND DOUBLERS IAW SRM 53-00-52.Nov 1, 2004 · N435US · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040922Duct · crackedPIT - Q1 - AIR DUCT, .5 INCH CRACK, LT RAM AIR DUCT UPPER SIDEWALL AT STA 540 AND S-22L. INSTALLED DOUBLER IAW TYP REP 53-50-03.Oct 31, 2004 · N435US · Boeing 7374B7 · Air Distribution SystemSDR USAA040928Clip · crackedPIT - Q1 - ATTACH CLIP, .5 INCH CRACK, STA 706, STR 1. REMOVED AND REPLACED WITH INDENT PART IAW SRM 51-40-02 AND 51-40-03.Oct 30, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040838Angle · crackedANGLE, 3 INCHES, CRACK, ANGLE, FWD SVC DOOR, INTERIOR STRUCTURE JUST BELOW WINDOW. REPLACED L ANGLE IAW SRM 51-40-02.Oct 30, 2004 · N776AU · Boeing 7374B7 · Service DoorsSDR USAA040927Clip · brokenPIT - Q1 - ATTACH CLIP, BROKEN, FRAME 706, STR S1. REMOVED BROKEN TIE CLIP AND REPLACED WITH SAME IAW SRM 51-40-02 AND 51-40-03.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040917Intercostal · crackedPIT - Q1 - MOUNT/INTERCOSTAL WITH 2 INCH CRACK AND 2 INCH BY 4 INCH CORRODED AREA, BS 727D TO BS 727E AT S 28L. REMOVED CORROSION, TREATED AND PRIMED. REPLACED INTERCOSTAL MOUNT IAW SRM 51-10-2.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040916Frame · crackedPIT - Q1 - FRAME, .2500 INCH CRACK, BS 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR IAW TYP REP 53-10-20A.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040912Frame · crackedPIT - Q1- FRAME, 1 INCH CRACK AND .7500 INCH CRACK (2 CRACKS) BS 616 AT S17L AND BS 616 AT S17R. CUT OUT DAMAGE, INSTALLED FILLERS AND NESTED ANGLES IAW TYP REP 53-62-01.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR SB04151Charger · inoperativePIT - MAINTENANCE REPORTED THE MID-CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY PACK AT SEAT ROW 21 OVERHEAD. OPERATIONAL CHECK GOOD.Oct 29, 2004 · N777AU · Boeing 7374B7 · Emergency LightingSDR USAA040921Bracket · crackedPIT - Q1 - BRACKET, 1 INCH CRACK, STA 927 AT 24.7L SUPPORT BRACKET. MANUFACTURED PART AND INSTALLED IAW SRM 51-41 AND MFG DWG 69771901.Oct 27, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040767Skin · crackedCLT, RON, SKIN- INCH CRACK, BS727E AT STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 231.Oct 26, 2004 · N430US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA200510004Skin · crackedA 1.5 INCH CRACK AT STA 727 BELOW ST 23 RT. REPAIRED IAW T/R 53-60-03.Oct 24, 2004 · N782AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040773Bulkhead · crackedPIT - C2, BULKHEAD SKIN, 1 INCH CRACK, FWD PRESSURE BULKHEAD RBL 57, WL 210. INSTALLED DOUBLER IAW SRM 53-10-08 FIG 211.Oct 24, 2004 · N777AU · Boeing 7374B7 · Fuselage Main, Bulkhead
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