Boeing 737-3B7

Service difficulty reports · 4,722

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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 = '7373B7'
  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 USAA041031Spar · damagedPIT - Q2 - SPAR, 2 INCHES X 1 INCH AREA, COMPOSITE DAMAGE/ DELAMINATION, LT AILERON, LEADING EDGE SPAR 34 INCH FROM OB END, UPPER FLANGE. INSTALLED REPAIR PLYS AND EXTRA IAW EA AND SRM.Nov 24, 2004 · N514AU · Boeing 7373B7 · AileronsSDR USAA041061Skin · gougedPIT - Q5 - SKIN SURFACE, 5 INCH LONG GOUGE, RUDDER LT SIDE STA 186, NEAR T/E. INSTALLED REPAIR PLYS IAW SRM.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041060Frame · separatedPIT - Q5 - CONDUCTIVITY FRAME, 15 INCHES X 12 INCHES, SEPARATION, RUDDER TOP LT SURFACE, UPPER LT CONDUCTIVITY FRAME SEPARATING FROM RUDDER. INSTALLED NEW CONDUCTIVITY FRAME IAW MM AND BAC 5010 AND DWG 65C25841.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Spar/RibSDR USAA041056Skin · damagedPIT - Q5 - SKIN SURFACE, SEVERAL AREAS OF 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041055Skin · chafedPIT - Q5 - SKIN SURFACE, 1.5 INCH LONG, TAPERING DEPTH, DEEP CHAFE WEAR, RUDDER LOWER RT L/E CORNER. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041054Skin · damagedPIT - Q5 - SKIN SURFACE, 3 INCH LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178 AND 13 INCHES FROM FWD SPAR. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041053Skin · chafedPIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041052Skin · chafedPIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040951Spoiler · delaminatedPIT - Q5 - SPOILER, 4 BY 6 INCH AREA, DELAMINATION. REMOVED AND REPLACED SPOILER IAW MM 27-62-91.Nov 23, 2004 · N516AU · Boeing 7373B7 · SpoilersSDR USAA040953Support Angle · crackedPIT - Q5 - SUPPORT ANGLE, .1250 INCH CRACK, STA 260 C/L. REPAIRED WITH NEW PART IAW MFG DWG 65-45833. REPAIRED WITH NEW PART IAW MFG DWG 65-45833.Nov 23, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA041073Skin · delaminatedPIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K)Nov 22, 2004 · N518AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040981Stringer · crackedPIT - Q5 - STRINGER, .25 INCH LONG CRACK AT STA 887 S-9L. INSTALLED (2) REPAIR ANGLES IAW TR 53-10-20A, 51-30-02, 51-40-09, 51-30-01.Nov 21, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR AWXA200401309Wire · brokenPHX - EEL - DURING 8-DAY CHECK FUNCTIONAL CHECK OF EMERGENCY LIGHTING FOUND THE EMERGENCY LIGHT AT SEAT ROW 2 LT INOPERATIVE, WIRES PULLED LOOSE FROM CONNECTORS. MAINTENANCE INSTALLED NEW WIRE HARNESS AT EMERGENCY LIGHT AT SEAT ROW 2 LT, OPERATIONAL CHECK WASNov 20, 2004 · N328AW · Boeing 7373B7 · Light System WiringSDR USAA040979Skin · crackedPIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537.Nov 18, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040978Skin · bulgedPIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537.Nov 18, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040977Skin · crackedPIT - Q5 - NR 6 SLAT SKIN, .1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Nov 17, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040976Support Angle · crackedPIT - C5 - SUPPORT ANGLE, 1 INCH LONG CRACK AT STA 540 S - 22L. SPLICE ANGLE IAW TYP REP 53-50-03.Nov 16, 2004 · N515AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040975Skin · corrodedPIT - Q6 - WING SKIN CUTOUT, .5 INCH X .75 INCH AT (4) LOCATIONS, CORROSION; NO LEVEL OR TASK; LT WING 7403L PANEL FUEL BOOST PUMP ACCESS AREA. REMOVED CORROSION AND REPAIRED IAW DRAFT EA 79514.Nov 16, 2004 · N516AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA040974Failsafe · crackedPIT - Q5 - FAIL SAFE CHORD, .75 INCH CRACK, STA 380 AT STR 15R. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11, FIG 1.Nov 16, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040980Stringer · crackedPIT - Q5 - STRINGER, .75 INCH CRACK, S-5A, BS 1138, INSTALLED DOUBLER IAW T/R 53-80-04 AND 53-00-01, FIG 221.Nov 15, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA040982Tie · crackedPIT - Q5 - STRINGER TIE, 1 INCH CRACK AT STA 827, S4L. DEFECTIVE PART REPLACED WITH IDENT PART.Nov 13, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA041059Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, 1 INCH X .2500 INCH AREA, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE STA 0 L/E. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041058Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, 3 INCHES LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178, 13 INCHES FROM FWD SPAR. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041057Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, SEVERAL AREAS 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040940Stringer Clip · crackedSTRINGER CLIP, .2500 INCH CRACK, BS 663.75, STRINGER 10 LT. DEFECTIVE PART REPLACED WITH IDENT PN.Nov 11, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR 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 USAA040983Structure · crackedPIT - Q5 - NR 4 SLAT, SEVERAL .1250 INCH TO .2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Nov 10, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040891Stiffener · crackedPIT- Q6 - VERTICAL STIFFENER, 1.2500 INCH CRACK, AT RBBL 6.15, STA 663.75. REPLACED VERTICAL STIFFENER IAW EA 79313 AND EO 5704V245 (RAFT).Nov 10, 2004 · N516AU · Boeing 7373B7 · Wing Main, Frame StructureSDR USAA040967Skin · corrodedPIT - Q6 - WING SKIN CUT OUT, 1.2500 INCH X .2500 INCH AT 4 LOCATIONS, CORROSION; NO LEVEL OR TASK, RT WING BOOST PUMP CUT OUT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM.Nov 9, 2004 · N516AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA040843Skin · crackedSKIN, .1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Nov 7, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR SB04152Pump · leakingBOS - FLT2039 - ON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, THE B SYSTEM HYDRAULIC FLUID BEGAN TO DECREASE AND THE B SYSTEM ENGINE DRIVEN PUMP LOW PRESSURE LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHNov 7, 2004 · N396US · Boeing 7373B7 · Hydraulic Pump (Electric/Engine), MainSDR USAA040984Bulkhead · crackedPIT - Q5 - WEB, 1 INCH CRACK, AT BS179, WL233.5, RBBL5.7 (178 BULKHEAD) WEB. INSTALLED DOUBLER IAW SRM 53-10-08, FIG 209 DETAIL II.Nov 5, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040905Attach Angle · crackedPIT - Q5 - ANGLE, 6 INCH LONG CRACK, HORIZ STAB CTR SECTION THRUST BEAM ATTACH ANGLE LT SIDE. REMOVED AND REPLACED ANGLE, REPLACED IAW TYP REP SRM 51-00-30. REMOVED AND REPLACED IAW TYP REP SRM 51-00-30.Nov 4, 2004 · N516AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA040947Strap · corrodedPIT - Q5 - STRAP, .2500 INCH BY .2500 INCH IN 66 AREAS, CORROSION; LEVEL 1; TASK NR-C53-107-02, AFT CARGO DOOR FRAME SECTION S25R, STA 807-848. REPLACED PART IAW SRM 53-00-07.Nov 3, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040903Angle · crackedHORIZ STAB CENTER SECTION THRUST BEAM ATTACH ANGLE RT SIDE. REMOVED AND REPLACED ANGLE IAW TYP REP REMOVED AND REPLACED SRM 51-00-30.Nov 3, 2004 · N516AU · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA040902Support Fitting · crackedPIT - Q5 - L/G SUPPORT FITTING, .2500 INCH CRACK, LT MLG SUPPORT FITTING AT REAR SPAR. REMOVED AND REPLACED WITH NEW FITTING IAW EO 5702V054.Oct 29, 2004 · N516AU · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR 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 USAA040944Skin · delaminatedPIT - Q5 - NR 2 SLAT SKIN, 3 INCH BY 4 INCH AREA, DELAMINATION, OB END T/E. REMOVED DAMAGE SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10.Oct 28, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR SB04150Odor · detectedPIT - FLT470 - ON CLIMB-OUT FROM PIT, EN ROUTE TO ORD, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE FORWARD GALLEY. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED ENGINE RUOct 28, 2004 · N390US · Boeing 7373B7 · Air Distribution FanSDR USAA040945Skin · delaminatedPIT - Q5 - SKIN TO CORE, 7 INCHES BY 2.5 INCH AREA DELAMINATED, IB RT AFT FLAP TOP SURFACE 34.5 INCHES- 42 INCHES FROM OB END. REMOVED UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER IAW SRM 51-70-10.Oct 27, 2004 · N516AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040900Skin · crackedPIT - Q5 - NR 4 SLAT SKIN, 6 FASTENER HOLES, .1250 INCH TO .2500 INCH CRACK. FASTENER HOLES, LOWER SKIN AREA BELOW ACTUATOR ATTACH POINT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, FIG 206.Oct 27, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040968Crease Beam · corrodedPIT - Q5 - CREASE BEAM WEB, .75 INCH (6 AREAS), CORROSION; NO LEVEL OR TASK, BETWEEN STA 420 AND STA 440, RT SIDES. CREASE BEAM WEB MFG IAW DWG 65-96956 AND BACD2003.Oct 26, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040943Skin · delaminatedSKIN AND CORE, 4 INCH BY 4 INCH AREA, IB T/E NR 4 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED DOUBLER, NEW CORE IAW 51-70-10.Oct 26, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040901Skin · crackedPIT - Q5 - SKIN, 1.5 INCH CRACK, FWD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-01.Oct 26, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040899Support Angle · crackedPIT - Q5 - SUPPORT ANGLE, 1 INCH LONG, CRACKED. SUPPORT DOWNLOCK VIEWER LT FWD CORNER, STA 259.5. REPLACED PART IAW DWG 65-45833.Oct 26, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB04149Charger · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD.Oct 26, 2004 · N528AU · Boeing 7373B7 · Emergency LightingSDR USAA040950Skin · gougedPIT - Q5 - SKIN, .025 INCH DEEP AND AT 10 INCHES LONG, GOUGED, STA 887-867, STR 1. CUT OUT DAMAGE INSTALLED SHIMS, FILLERS, STRAPS, DOUBLER AND TRIPLER IAW EA 79291.Oct 25, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040889Floorbeam · mismanufacturedPIT-Q5- FLOORBEAM, INCORRECT MATERIAL FROM MFG. FLOORBEAM UPPER CHORD REMOVED AND REPLACED IAW EA 68822A, FLOOR STA 328.Oct 25, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR 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/Skin
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