N383US, cancelled Jul 25, 2006

Service difficulty reports · 151

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N383US' AND deregistration_id = 'N383US-2006-07-25'
  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 SB05119Adc · failedCLT FLT448 ON TAKEOFF ROLL, WITH FIRST OFFICER FLYING, THE FIRST OFFICER LOST AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED. AFTER TRANSFER OF CONTROLS TO CAPTAIN, THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DESep 23, 2005 · N383US · Boeing 7373B7 · Air Data ComputerSDR USAA050464Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH LONG, BS 747 BETWEEN 19L AND 20L. INSTALLED DOUBLER SKIN REPAIR PER EA 83173, SRM 53-00-01. (M)Apr 2, 2005 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05036Pressure Switch · faultyBWI - FLT141 - EN ROUTE FROM DCA TO IND, AT FL270, WITH THE APU POWERING THE NR 2 GENERATOR BUS, THE APU LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY AN APU AUTO SHUT DOWN. THE NR 2 ENGINE CSD WAS ALREADY ON MEL SO THE FLIGHT DIVERTED TO BWI AND LANDED WITHMar 3, 2005 · N383US · Boeing 7373B7 · APU Oil SystemSDR SB05027Battery Pack · dischargedPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ABOVE THE AFT LEFT SERVICE DOOR AND THE AFT RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD.Feb 18, 2005 · N383US · Boeing 7373B7 · Emergency LightingSDR SB04169Logic Card · dirtyALB - FLT1231 - ON APPROACH TO ALB FROM CLT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. CREW PERFORMED MANUAL GEAR EXTENSION PROCEDURE AND RECEIVED ALL THREE GREEN GEAR LIGHTS. CREW REPORTED LIGHTS TESTED OK. FLIGHT LDec 21, 2004 · N383US · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA040866Skin · crackedSKIN, 1.75 INCHES CRACKED AT STA 927 AND 947.5 AT STR 25R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01.Nov 11, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040786Floor Support · corrodedPIT - Q5, FLOOR SUPPORT, .1250 INCH BY .1250 INCH AREA, CORROSION; LEVEL 1; TASK NRC53-107-02, FASTENER HOLE AT STA 947 RBL 20. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, SHIM AND FILLER IAW EA 79192.Oct 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040798Channel · crackedPIT, Q5, CHANNEL, 6 INCH LONG CRACK, NR 2 PYLON LOWER CHANNEL NAC STA 363. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02.Oct 29, 2004 · N383US · Boeing 7373B7 · Nacelle/Pylon Miscellaneous StructureSDR USAA040782Skin Panel · damagedPIT, Q5, SKIN PANEL, REMOVED AND REPLACED SKIN PANEL AT BS 980 FROM S20R-S25R. REMOVED AND REPLACED SKIN PANEL DUE TO TEMPORARY REPAIRS; REPAIR TOO CLOSE TO LAP JOINTS; IAW EO 79060.Oct 23, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR 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 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 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 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 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 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 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 StructureSDR USAA040788Keelbeam · corrodedPIT Q5, KEEL BEAM, 2 INCHES X 40 INCHES AREA CORROSION; LEVEL 1 TASK NR C53-208-01, L KEEL BEAM STA 500D-540. REMOVED AND REPLACED, SPLICED IN NEW SECTION IAW TYP REP 53-60-09.Sep 25, 2004 · N383US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040802Skin · crackedPIT, Q5, SKIN, 6 INCH CRACK, RT PYLON LOWER PAN FROM NAC 319 AFT TO END. REMOVED AND REPLACED SKIN AND INSTALLED DOUBLER IAW SRM 51-70-13.Sep 21, 2004 · N383US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA040781Intercostal · damagedPIT, Q5, INTERCOSTAL, HOLE DAMAGE. LIGHTENING HOLE DAMAGE, STA 294.5 + 312 LBL 10 INCH INTERCOSTAL FLOORBEAM LIGHTENING HOLE DAMAGE. FABRICATED WEB AND INSTALLED SAME IAW 53-10-51, FIG 1, PG 17.Sep 16, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040792Angle · corrodedPIT, Q5, KEEP REPAIR ANGLE, 20 INCH AREA, CORROSION; LEVEL 1; TASK NR C 53-208-01 R KEEL STA 520-540. INSTALLED NEW REPAIR ANGLE/ DOUBLER IAW SRM 51-70-11.Sep 14, 2004 · N383US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA040805Door Frame · crackedPIT, Q5, WEB FRAME, 3 INCH CRACK AT FWD ENTRY DOOR LOWER WEB FRAME FORWARD CORNER. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-02 FIG 1, SRM 51-70-11 FIG 1.Sep 13, 2004 · N383US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040787Floor Support · corrodedPIT, Q5, FLOOR SUPPORT, 4 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02 FLOOR SUPPORT, STA 986.5 RT BL0. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-60-51.Sep 12, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040797Angle · corrodedPIT, Q5, Z-ANGLE, 4 INCHES LONG, CORROSION; LEVEL 1 TASK NR C53-107-01 AFT ENT DOOR Z-ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG.Sep 12, 2004 · N383US · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA040824Keelbeam · crackedPIT - Q5, KEEL REPAIR ANGLE, .2500 INCH CRACK, FASTENER HOLE, STA 520 ON KEELBEAM REPAIR ANGLE RT. REPAIR ANGLES/DOUBLER INSTALLED IAW SRM 51-70-11.Sep 11, 2004 · N383US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA040803Skin · delaminatedPIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10.Sep 10, 2004 · N383US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040804Skin · delaminatedPIT, Q5, TOP SKIN - CORE BOND 1 INCH AREA, DELAMINATION, LT WING NR 1 SPOILER AT AFT OB CORNER - TOP SURFACE. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.Sep 10, 2004 · N383US · Boeing 7373B7 · SpoilersSDR USAA040808Skin · delaminatedPIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10.Sep 10, 2004 · N383US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040807Spar · crackedPIT, Q5, ANGLE SUPPORT .7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100.Sep 9, 2004 · N383US · Boeing 7373B7 · Vertical Stabilizer, Spar/RibSDR USAA040806Skin · debondedPIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10.Sep 8, 2004 · N383US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040796Floor Support · corrodedPIT, Q5, FLOOR SUPPORT 1 INCH 10 INCH AREA. CORROSION; LEVEL 1; TASK NR C53-107-02 LOCATED AT STA 986.5 TO 1016, RBL 3.54 TO RBL 18.25. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Sep 5, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040809Skin · delaminatedPIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INSTALLED NEW TOP SKIN IAW SRM 51-70-10.Sep 3, 2004 · N383US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040815Clip · crackedPIT, Q5, CLIP 1 INCH CRACK, STR 19 AND STA 986 BULKHEAD. INSTALLED CLIP IAW SRM 5-40-02.Sep 1, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040820Crease Beam · crackedPIT, Q5, CREASE BEAM WEB 1 INCH CRACK. LT CREASE BEAM BS 616-639. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Sep 1, 2004 · N383US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050822Skin · wornMID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FIG 208.Sep 1, 2004 · N383US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040783Stringer Clip · crackedPIT - Q5, TIE- .1250 INCH CRACK, RIVET, STR TO FRAME CLIP, STA 663.75-S10R. REMOVED AND REPLACED STRINGER CLIP (TIE) IAW 53-00-03.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040812Clip · crackedPIT, Q5, CLIP EST. .125 INCH STA 500D S 8L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040813Clip · crackedPIT, Q5, CLIP EST. .125 INCH CRACK, STA 500B S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040814Clip · crackedPIT, Q5, CLIP EST. .125 INCH CRACK, STA 440S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040823Clip · crackedCLIP, EST. .125 INCH CRACK, STA 500D SGL. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040810Stringer Clip · crackedPIT, Q5, STRINGER CLIPS, .5000 INCH AND .1250 INCH CRACKS, STA 578, STR S9R. CLIP REPLACED IAW SRM 51-40-02.Aug 28, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040819Skin · crackedPIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Aug 28, 2004 · N383US · Boeing 7373B7 · Leading Edge Devices
Back to N383US, cancelled Jul 25, 2006