Boeing 737-3B7

Service difficulty reports · 4,722

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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"

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SDR USAA040793Threshold · corrodedPIT,Q5, THRESHOLD, 2 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01 AFT CARGO DOOR THRESHOLD S25R. INSTALLED THRESHOLD IAW DWG 65-47957. AFT CARGO DOOR THRESHOLD S25R.Oct 23, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040795Frame · corrodedPIT, Q5, FRAME .2500 INCH X .2500 INCH- 6 EA AREAS, CORROSION; LEVEL 1; TASK NR C53-208-01 AROUND FASTENER HOLES - STA 847 FRAME BETWEEN S26R, ES25R. SPLICED IN NEW FRAME SECTION IAW EA 79270.Oct 23, 2004 · N383US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040948Frame · corrodedPIT - Q5 - ANTENNA MOUNT FRAME, 3 INCHES L BY 1 INCH W, CORROSION; LEVEL 1; TASK NR C53-107-01, VHF ANTENNA NR 2 MOUNT. REPAIRED IAW SM 51-10-2 AND 51-40-00.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040946Floor Panel · corrodedPIT - Q5 - FLOOR PANEL, 1 INCH BY 5 INCH AREA CORROSION, LEVEL 1; TASK NR C53-107-02, PANEL NR 99, STA 1016. REPLACED FLOOR PANEL NR 99 IAW SRM 51-70-12.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Floor PanelSDR USAA040941Channel · crackedPIT - Q5 - CHANNEL, .5 INCH CRACK, STA 540 LBBL 0, RBBL U CHANNEL. REPLACED CHANNEL IAW SRM 53-00-03.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040888Pan · tornPIT, Q5, FLOOR PAN, .5 INCH TEAR, LBL 18 INCH AT STA 986.5. INSTALLED FILLER/DOUBLER IAW SRM 51-70-13, FIG 1.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB04147Battery Pack · dischargedFOUND EXTERIOR EMERGENCY LIGHTS OVER R1 AND L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK.Oct 21, 2004 · N524AU · Boeing 7373B7 · Emergency LightingSDR USAA040764Skin · crackedCLT, RON, SKIN-1 INCH CRACK, BS 727E AT STRINGER 22R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229.Oct 20, 2004 · N374US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040949Support Angle · corrodedPIT - Q5 - SUPPORT ANGLE, 1.2500 INCH BY .5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, FLOOR SUPPORT, STA 859. BURNISHED, TREATED AND PRIMED IAW TYP REP 53-10-06B.Oct 19, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040898Door Frame · crackedPIT - Q5 - FRAME, .5 INCH CRACK. FWD SERVICE DOOR SURROUND FRAME AT 294.5 AND S17R. FABRICATED DOUBLER IAW SRM 51-70-11.Oct 19, 2004 · N516AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA040890Stiffener · crackedPIT- Q5 - VERTICAL STIFFENER, .7500 INCH CRACK, VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERT STIFFENER IAW EA 79313/ EO5704V245 (DRAFT).Oct 19, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040829Skin · delaminatedPIT - C4, IB AFT FLAP SKIN, 3 INCHES BY 2.5 INCH AREA, DELAMINATION, IB AFT FLAP OB T/E LEFT WING. REMOVED SKIN AND CORE, INSTALLED REPAIR AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10.Oct 19, 2004 · N385US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040837Skin · delaminatedPIT - C4, IB AFT FLAP SKIN, 3 INCHES X 2.5 INCHES AREA, DELAMINATION. IB AFT FLAP OB T/E LT WING. REMOVED DELAMINATION, INSTALLED REPAIR CORE, SKIN AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10.Oct 19, 2004 · N385US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040794Intercostal · corrodedPIT, Q5, INTERCOSTAL, .5000 INCH AND .2500 INCH, 2 BRACKETS, CORROSION; NO LEVEL OR TASK. E11 DOOR FRAME AT SWITCH NR 3196 INSIDE OF FRAME, BL0, STA 203.8. FABRICATED ANGLES, REPLACED IAW SRM 53-00-04.Oct 19, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040897Frame · crackedPIT- Q5 - FRAME, 2 INCH CRACK, STA 440 S9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A.Oct 18, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040827Pressure Blkhd · damagedPIT - Q5, AFT PRESSURE BULKHEAD, NUMEROUS TENSION BOLTS LOOSE, STA 1016 AFT PRESSURE BULKHEAD. REPLACED TENSION BOLTS IAW EA 79074 AND SB 737-53-1229.Oct 18, 2004 · N383US · Boeing 7373B7 · Fuselage Main, BulkheadSDR SB04146Light · inoperativeCLT - PILOT REPORTED THE EMERGENCY EXIT ROW EVACUATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD.Oct 17, 2004 · N390US · Boeing 7373B7 · Emergency LightingSDR SB04145Windshield · crackedPHL - FLT 1447 - EN ROUTE FROM PHL TO ATL, AT FL270, CAPTAIN REPORTED VIA ACARS THE L1 WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO PRESSURIZATION PROBLEMS WERE ENCOUNTERED AND NO EMERGENCY WAS DECLARED. MAINTEOct 16, 2004 · N384US · Boeing 7373B7 · Flight Compartment WindowsSDR USAA040893Stringer Clip · crackedPIT- Q5- STRINGER TIE CLIP, .2500 INCH CRACK, BS 344, STR8, RT. FABRICATED IAW MFG DWG 66-244553 AND INSTALLED IAW SRM 51-40-01.Oct 15, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040892Stringer Clip · crackedPIT- Q5- STRINGER TIE CLIP, 1.25 INCH CRACK, BS 360, STR 4, RT. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM 51-10-02.Oct 15, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040750Skin · crackedPIT, C3; SKIN, .2500 INCH CRACK, BETWEEN STR 13/16R AND FRA 947.5. 11 INCH W X 9.5 INCH H FILLER, ALONG WITH 10 INCH W X 13.5 H DOUBLER IAW SRM 53-60-01, FIG 207.Oct 15, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040896Angle · crackedPIT - Q5 - ANGLE, .5 INCH CRACK, STA 380 AT STR 15R. FABRICATED REPAIR ANGLE IAW SRM 51-70-11.Oct 14, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040830Skin · delaminatedPIT - C2, UPPER AND LOWER SKIN, .5 INCH BY 2.5 ALONG T/E, DELAMINATED, IB T/E OF RT OB AFT FLAP. FABRICATED REPAIR SKIN AND DOUBLER AND NEW IAW TR 57-50-39A AND EO 5796X105.Oct 14, 2004 · N504AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040828Tee Fitting · defectiveSTRINGER T FITTING, NO EDGE DISTANCE. NO EDGE DISTANCE FOR FASTENERS, FWD SIDE AFT PRESSURE BULKHEAD AT S10L. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-49914, DASH NR 535, EA 79074.Oct 13, 2004 · N383US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040755Window Frame · crackedPIT, C5, WINDOW FRAME, .2500 INCH CRACK, CAPTAINS WINDOW POST BETWEEN NR 1 AND NR 2 WINDOWS TOP, FWD CORNER. INSTALLED DOUBLER IAW SRM, FIG 103.Oct 12, 2004 · N521AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040754Keelbeam · crackedPIT, C5, KEELBEAM, 2 INCH LONG CRACK, KEELBEAM RT SIDE JUST AFT OF STA 540. INSTALLED REPAIR ANGLE IAW EA 79268.Oct 12, 2004 · N521AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA040895Tie Clip · crackedPIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 663 STRINGER 2 RT. FABRICATED NEW CLIP IAW DWG 69-45156 IAW SRM 51-40-02.Oct 11, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040745Pressure Panel · crackedPIT, C5; PRESSURE PANEL, 2 INCH CRACK. LT WHEEL WELL UPPER DECK, 30 INCH LT OF BL0. INSTALLED DOUBLER AND SHIMS IAW TYP REP 53-60-04A AND EA 79277.Oct 11, 2004 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040744Skin · gougedPIT, C5; SKIN WITH .5 INCH GOUGE, STA 767 AT 22L JUST BELOW STRINGER. DRILLED HOLE TO .250 INCH DIA, INSTALLED RIVET WET IAW SRM 53-00-01, FIG 219.Oct 11, 2004 · N521AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040747Bulkhead · crackedPIT, C1; WEB SKIN, .2500 INCH CRACK, FWD BULKHEAD, STA 178, WEB STA 212. INSTALLED DOUBLER REPAIR IAW EO 5300V153.Oct 10, 2004 · N504AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040746Stiffener · crackedPIT, C5; STIFFENER ANGLE, 3.5 INCH CRACK, LOWER AFT CORNER OF CARGO DOOR IN STIFFENER ANGLE. DEFECTIVE PART REPLACED WITH IDENT PN IAW JOB CARD J3-51-52301.Oct 10, 2004 · N521AU · Boeing 7373B7 · Cargo/Baggage DoorsSDR SB04142Light · looseCLT - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE IN SOCKET. SECURED BULB. OPERATIONAL CHECK GOOD.Oct 10, 2004 · N392US · Boeing 7373B7 · Emergency LightingSDR USAA040825Frame · crackedPIT - Q5, FRAME, CRACKED, (2EA) 2 INCHES AND 2.2500 INCH, 727D BETWEEN S-27L AND S-27R AT 1 RBBL AND LBBL. REPAIRED DOUBLER IAW SRM 51-70-11.Oct 8, 2004 · N383US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040834Skin · crackedSKIN, 1 INCH CRACK, BS 727D, STR 22R. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01.Oct 8, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040752Keelbeam · corrodedPIT, C1, KEELBEAM, 1 INCH X 20 INCH AREA, CORROSION; NO LEVEL OR TASK, BS520-540 AT STR 26L. REMOVED CORROSION, INSTALED NESTED REPAIR ON ONE SIDE ONLY IAW SRM 51-70-12, DET III.Oct 8, 2004 · N395US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA040748Bulkhead · crackedPIT, C1; SKIN WITH .5 INCH LONG CRACK AT AFT PRESSURE BULKHEAD AT BL0 AND 10 INCHES ABOVE CENTER. INSTALLED DOUBLER IAW SRM 53-80-08.Oct 7, 2004 · N385US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040749Skin · crackedPIT, C3; SKIN, (3 EA) CRACKS; 1 INCH, 2.7 INCHES AND 1 INCH, AFT OF 727E-747, S18R. INSTALLED REPAIRS IAW SRM 53-00-01, FIG 228.Oct 6, 2004 · N385US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040701Floor Support · bentSUPPORT, .2500 INCH X 20 INCH AREA, BENT/LIFTING METAL, BS540 BETWEEN IB AND OB SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-2.Oct 6, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040942Skin · delaminatedPIT - Q5 - NR 2 SLAT, 2 SQ INCH AREA, DELAMINATION, IB T/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10.Oct 2, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040826Attach Fitting · chafedPIT - Q5, FITTINGS, .1250, .5, .5, .5 INCH AREAS, HEAVY CHAFING (4 AREAS), ALL 4 AFT LUGS OF VERT STAB ATTACH FITTINGS.Oct 2, 2004 · N383US · Boeing 7373B7 · Vertical Stabilizer, Attach FittingsSDR USAA040785Seat Track · corrodedPIT - Q5, SEAT TRACK, 2 INCH BY 4 INCH CORRODED AREA, LEVEL 1 TASK NR C53-107-02, AFT END OF RT OB SEAT TRACK, STA 947. MANUFACTURED FILLERS AND SPLICED IN A NEW SECTION IAW SRM 53-00-52.Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040789Floorbeam · corrodedPIT - Q5, FLOORBEAM TEE CAP, .1250 INCH BY .1250 INCH (6 AREAS), CORROSION; LEVEL 1; TASK NR C53-107-02, TOPS OF FLOORBEAMS IN AROUND SCREW HOLES STA 1016-986.5. REMOVED CORROSION, TREATED, PRIMED, REPLACED 10 INCHES OF T-CAP IAW SRM 53-60-51.Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA040790Channel · corrodedPIT,Q5, Z-CHANNEL, 4 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SERVICE DOOR Z-CHANNEL. REMOVED AND REPLACED IAW SRM 51-40-02.Oct 2, 2004 · N383US · Boeing 7373B7 · Service DoorsSDR USAA040799Floorbeam · crackedPIT, Q5, FLOORBEAM, 3 INCH CRACK (BROKEN) .400 INCH CRACK, STA 540 LBL 1 AND LBL 19 SUPPORT). REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 53-21-00.Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA040800Bracket · crackedPIT, Q5, BRACKET, 1 INCH X .2500 INCH CRACK, (L) BRACKET, STA 350 RBL 20. FABRICATED NEW BRACKET IAW DWG 69-74588.Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040801Floor Support · crackedPIT, Q5, FLOOR SUPPORT WITH .2500 INCH X .3750 INCH CRACKS, END OF FLOOR SUPPORT, STA 540 LT AND RT OF BL-0. REMOVED AND REPLACED IAW SRM 53-21-00.Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB04137Proximity Sensor · faultyEWR - FLT 2164 - ON DESCENT INTO LGA FROM DCA, CREW RECEIVED A NR 4 LEADING EDGE KRUGER FLAP AMBER LIGHT ALONG WITH A LEADING EDGE TRANSIT AMBER LIGHT DURING SLAT EXTENSION. CREW RECYCLED FLAPS IN HOPES OF CLEARING THE PROBLEM WITH NO HELP. CREW DECIDED TO DOct 2, 2004 · N385US · Boeing 7373B7 · Leading Edge Slat Position Indicating SystemSDR USAA040784Skin · crackedPIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01.Oct 1, 2004 · N383US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040791Floor Support · corrodedPIT, Q5, ANGLE/TRACK, 2 INCH CORROSION, LEVEL 1; TASK NR C53-202-01 AFT CARGO CORE, FLOOR TIE DOWN TRACK, STA 859 LBL 17.20. SPLICED REPAIR SECTION INTO FLOOR TRACK IAW SRM 53-00-53.Sep 30, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040821Channel · crackedPIT, Q5, CHANNEL WITH A 4 INCH LONG CRACK IN LOWER CHANNEL AT NR 2 NAC, STA 345. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02.Sep 30, 2004 · N383US · Boeing 7373B7 · Nacelle/Pylon Miscellaneous Structure
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