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 USAA050439Support Angle · crackedCLT - Q6 - SUPPORT ANGLE, (.075 INCH) CRACK, STRINGER 11R, STATION 354. INSTALLED NEW ANGLE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050438Stringer · crackedCLT - Q6 - STRINGER, (.250 INCH CRACK), STRINGER 4L, STATION 908.0906. INSTALLED SPLICE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA050437Stringer · crackedCLT - Q6 - STRINGER, (.250 INCH CRACK) STRINGER 4R STA 908.0903. INSTALLED SLICE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA050436Stringer Clip · crackedCLT - Q6 -TIE CLIP, (.5 INCH CRACK), STATION 578.0991, STRINGER 8R. REPLACED TIE CLIP IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR SB05043Power Supply · failedBDL - MAINTENANCE REPORTED ALL THE EMERGENCY LIGHTS CONTROLLED BY POWER SUPPLY M1479 WERE EXTREMELY DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY M1479. OPERATIONAL CHECK OF LIGHTS GOOD.Mar 31, 2005 · N439US · Boeing 7374B7 · Emergency LightingSDR USAA050571Structure · damagedCLT - FOUND NR 1 SLAT, NR 1 SLAT LOWER NOSE SURFACE T/E AT AFT ROW OF FASTENERS. REPAIR PCW IAW SRM 57-43-01. (M)Mar 30, 2005 · N439US · Boeing 7374B7 · Leading Edge DevicesSDR USAA050431Floorbeam · corrodedCLT - Q4 - FLOORBEAM, (.5 INCH) CORROSION. STA 312, BL 0 TO RBL 10. SPLICED IN NEW T-CAP IAW SRM. (K)Mar 30, 2005 · N440US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050457Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH DIAMETER, STATION 312 BL 0 TO BL 10 RT. SPLICED IN NEW T-CAP IAW SRM 53-10-51. (M)Mar 29, 2005 · N440US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050428Skin · crackedCLT - Q6 - EXTERNAL SKIN, 1 INCH, CRACKED, FWD CARGO DOOR HANDLE CUTOUT. (K)Mar 29, 2005 · N442US · Boeing 7374B7 · Cargo/Baggage DoorsSDR SB05041Charger · inoperativeCLT - FOUND FORWARD SERVICE DOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY.Mar 29, 2005 · N780AU · Boeing 7374B7 · Emergency LightingSDR USAA050430Skin · damagedCLT - Q6 - RUDDER SKIN, (.5 INCH X .5 INCH) COMPOSITE DAMAGE, RUDDER T/E STA 151. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K)Mar 28, 2005 · N442US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA050429Skin · crackedCLT - Q6 - EXTERNAL SKIN, (1 INCH CRACK), AFT CARGO DOOR HANDLE CUTOUT. INSTALLED DOUBLER. (K)Mar 28, 2005 · N442US · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA050390Rib · crackedCLT - Q6 - RIB, (1.5 AND .3750 INCH) CRACK; H WING, ROB AT WS 505 UPPER FLANGE RADIUS 20 INCH FROM L/E OF RIB. INSTALLED REPAIR DOUBLER IAW EA. (K)Mar 24, 2005 · N442US · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA050427Attach Angle · wornCLT - Q4 - ATTACH ANGLE, (.75 INCH X .50 INCH) WORN, LT HORIZONTAL STABILIZER TIP BL249-81. REPLACED WITH FABRICATED ANGLE IAW SRM. (K)Mar 16, 2005 · N440US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA050377Tie Clip · crackedCLT - Q6 - TIE CLIP, SRM 51-10-02, CRACKED, STA 787, STR 24R. REPLACED TIE CLIP. (K)Mar 16, 2005 · N442US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050376Frame · crackedCLT - Q6 - FRAME, .125 INCH, CRACKED, STA 787, STR8/9L. INSTALLED DOUBLER IAW TR 53-10-20B. INSTALLED DOUBLER IAW TR. (K)Mar 16, 2005 · N442US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050360Tie Clip · crackedCLT - Q6 - TIE CLIP, .250 INCH CRACK, STR 4R, BS 867. REPLACED TIE CLIP IAW SRM. (K)Mar 15, 2005 · N442US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050361Tie Clip · crackedCLT - Q6 - TIE CLIP, .250 INCH CRACK, STR 10L, BS 685. REPLACED TIE CLIP IAW SRM. (K)Mar 15, 2005 · N442US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050362Frame · crackedCLT - Q6 - FRAME, .250 INCH CRACK, STA 867, STR 8/9L. INSTALLED DOUBLER REPAIR IAW TR. (K)Mar 15, 2005 · N442US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050410Skin · crackedCLT - Q6 - FUSELAGE SKIN, (.5 INCH) CRACK., RT WW BEADED PRESSURE DECK STA 664RBL 40. INSTALLED FILLERS AND TRIPLER IAW TR. (K)Mar 12, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050411Rib · crackedCLT - Q6 - RIB, (2 EA- 1.5 INCH AND .3750 INCH) CRACK. LT WING RIB AT WS 505 UPPER FLANGE RADIUS 20 INCHES FROM L/E OF RIB. FABRICATED REPAIR DOUBLER IAW EA. (K)Mar 10, 2005 · N442US · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA050350Skin · damagedCLT - Q6 - SKIN, 2.25 INCH X 7 INCH, PREVIOUS REPAIR, SCAB PATCH, STATION 178, STRINGER 17L. SPLICE STRAP INSTALLED IAW EO 5300V157. (K)Mar 10, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050349Skin · crackedCLT - Q6 - SKIN, 2.25 INCH X 7 INCHES. PREVIOUS REPAIR, SCAB PATCH INSTALLED, STATION 178, STRINGER S17R. INSTALLED SPLICE STRAP IAW EO 5300V157. (K)Mar 10, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050347Angle · crackedCLT - C2 - ANGLE, .250 INCH CRACK, CLOSE-OUT WEB JUST OB OF LT AILERON QUADRANT. REPLACED WITH FABRICATED ANGLE IAW SRM 51-10-02. (K)Mar 7, 2005 · N781AU · Boeing 7374B7 · AileronsSDR USAA050345Angle · crackedCLT - Q6 - ANGLE, .025 INCH CRACK, STATION 500G-520 BL0. REPLACED WITH FABRICATED PART IAW SRM 51-30-01, DWG NR 69-35365, AND SRM 51-10-02. (K)Mar 7, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050341Stringer Clip · crackedCLT - Q6 - STRINGER CLIP, .5 INCH CRACK, STATION 500A, STRINGER 16R. REPLACED WITH FABRICATED CLIP IAW SRM. (K)Mar 4, 2005 · N442US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA050355Spar · chippedPIT - Q4 - RUDDER L/E SPAR, .2500 INCH X .1250 INCH DEEP CHIP IN EDGE CHIP, LT L/E SPAR TAB. BLEND OUT REPAIR, HFEC INSPECTION AND VISUAL, SEALED IAW EA 79967. (K)Mar 3, 2005 · N438US · Boeing 7374B7 · Rudder, Spar/RibSDR USAA050358Skin · damagedPIT - Q4 - COMP SKIN LT ELEVATOR, 2.5 INCH LENGTH X .125 INCH WIDTH, COMPOSITE DAMAGE, STA 55 AT PANEL CENTER TOP SURFACE LT ELEV. INSTALLED REPAIR PLIES IAW SRM AND EA. (K)Mar 2, 2005 · N438US · Boeing 7374B7 · Elevator, Plate/SkinSDR USAA050338Attach Angle · crackedCLT - Q6 - ATTACH ANGLE, .250 INCH CRACK, STATION 578 BETWEEN STRINGERS 8R AND 9R. REPLACED ATTACH ANGLE WITH FABRICATED PART IAW DWG.Mar 2, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050337Stringer Clip · crackedCLT - Q6 - TIE CLIP, .3750 INCH CRACK, STA 827, STRINGER 3R. REPLACED TIE CLIP IAW SRM. (K)Mar 2, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050336Stringer Clip · crackedCLT - Q6 - STRINGER CLIP, .5 INCH CRACK, STATION 706, STRINGER 11R. REPLACED TIE CLIP IAW SRM 51-10-02.Mar 2, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050333Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 8 INCH AREA, FORWARD ENTRANCE FLOOR SUPPORT. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)Mar 1, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050325Skin · puncturedPIT - FOUND SKIN PUNCTURED .5 INCH BY .5 INCH, BS 727A PLUS 10 AT BL 0. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 79988. (M)Feb 25, 2005 · N438US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050353Skin · chafedPIT - Q4 - SLAT, 8 INCH LONG X 3 INCH WIDE AREA, CHAFED. NR 4 SLAT IB T/E LOWER SKIN SURFACE. INSTALLED FILLER AND INTERNAL DOUBLER, KEY CORE AND TOP DOUBLER, SEALED EDGE AND REFINISHED IAW SRM. (K)Feb 24, 2005 · N438US · Boeing 7374B7 · Leading Edge DevicesSDR USAA050304Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 101 INCH BY 2 INCH, STATION 312 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM IAW SRM 53-10-51. (M)Feb 23, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050335Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 8 INCHES, STATION 312. CORROSION LEVEL 1, TASK C53-107-01. REMOVED AND REPLACED PER SRM AND IPC 53-4200 FIG 2. (M)Feb 23, 2005 · N438US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050328Channel · crackedPIT - FOUND CARGO FLOOR CHANNEL AND SUPPORT ANGLE WITH CRACKS, APPROX .5 INCH CRACKS, FS 500G, RBBL 6. MANUFACTURED AND INSTALLED CARGO FLOOR CHANNEL AND SUPPORT ATTACH ANGLE PER SRM 53-00-53. (M)Feb 23, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050302Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 101 INCHES, STATION 344 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. (M)Feb 23, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050303Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 10.9 INCHES BY 2 INCHES, STATION 328 ENTIRE T-CAP. INSTALLED T-CAP REPAIR PER SRM 53-10-51. (M)Feb 23, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050301Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCH BY 78 INCH AREA OF CORROSION, STATION 294 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. (M)Feb 23, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050327Support · crackedPIT - FOUND ANTENNA SUPPORT CRACKED 1.5 INCH, 1 INCH, .6250 INCH AT STATION 727D S27L AND S27R. FABRICATED REPAIR ANGLE, TRIMMED, FITTED, HEAT TREATED PER SRM 53-60-01. (M)Feb 23, 2005 · N438US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050357Skin · delaminatedPIT - Q4 - EXT COMPOSITE SURFACE, .500 INCH AREA OF DELAMINATION, LT ELEVATOR TAB TOP IB CORNER. PREPARED DAMAGED AREA, INSTALLED REPAIR PLYS, HARDWARE, REFINISHED IAW SRM 55-20-01 AND 51-70-05. (K)Feb 22, 2005 · N438US · Boeing 7374B7 · Elevator, Tab StructureSDR USAA050307Skin · crackedPIT - FOUND NR 2 SPOILER CRACKED .125 INCH, AND .5 INCH BY .5 INCH AREA DELAMINATED. REMOVED AND REPLACED PER M/M 27-61-11 AND 27-61-11 AND 27-61-51. (M)Feb 22, 2005 · N440US · Boeing 7374B7 · SpoilersSDR SB06019Charger · faultyCLT DURING ELECTRIC POWER INTERRUPTION AT GATE, CREW REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED. FLIGHT ATTENDANT NOTICED NUMEROUS FLOOR AND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THAT WHEN THE EMERGENCY LIGHTS ARE PLACED IN TEST MODE, Feb 20, 2005 · N445US · Boeing 7374B7 · Emergency LightingSDR USAA050329Angle · crackedPIT - FOUND ANGLE CRACKED .25 INCH, S14R TO S15R AT BS 360 ANGLE BETWEEN STRINGERS. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M)Feb 20, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050324Floorbeam · corrodedPIT - FOUND BEAM WITH CORROSION 48 INCH LONG SEVERAL AREAS, FS 312, UPPER CAP FLOORBEAM. CORROSION LEVEL 1, TASK C53-107-01. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-51, FIG 205. (M)Feb 20, 2005 · N438US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050332Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, STATION 616 FRAME JUST BELOW FLOOR. DOUBLER INSTALLED PER TYPICAL REPAIR 53-62-01. (M)Feb 20, 2005 · N438US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050326Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, JUST BELOW FLOOR ON FRAME 616L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01. (M)Feb 20, 2005 · N428US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050334Channel · corrodedPIT - FOUND ZEE CHANNEL CORRODED 1 INCH BY 12 INCH AREA, RIGHT SIDE ZEE CHANNEL STATION 294-362. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01, 51-40-00. (M)Feb 19, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050359Support Bracket · corrodedPIT - Q4 - BRACKETS, 1 INCH X 3 INCH CORROSION, 4 BRACKETS. CORROSION; LEVEL 1; TASK C53-107-02 THRESHOLD SUPPORT BRAKETS, FWD DOOR ENTRY FLOOR STRUCTURE. PARTS REPLACED IAW MFG DWG. (K)Feb 18, 2005 · N438US · Boeing 7374B7 · Fuselage Miscellaneous Structure
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