Boeing 737-33A

Service difficulty reports · 1,809

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 = '73733A'
  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 AWXA0001791Plate · crackedTOP LEFT PYLON LAND FOR ACCESS PANEL CRACKED NAC STA 214. REPAIRED IAW AWA ER 03-5433-00340-DL1.May 30, 2001 · N168AW · Boeing 73733A · Nacelle/Pylon, Plate/SkinSDR AWXA0001790Frame · crackedFWD CARGO DOOR PAN FRAME CRACKED 3 INCHES NEAR HOLD OPEN HOOK. REMOVED AND REPLACED FWD CARGO DOOR, FWD LWR CORNER PAN IAW SRM 51-40-05 PG 1-2 AND 51-40-02 PG 2-4.May 30, 2001 · N168AW · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA0001789Beam · crackedCRACK IN FWD CARGO DOOR LWR BEAM 1 INCH THROUGH FASTENER HOLE COMMON TO LWR TEE AND BEAM AT 4TH FASTENER HOLE BS 444. REPAIRED IAW AWA ER 03-5231-01130-DL1.May 30, 2001 · N168AW · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA0001788Crossbeam · crackedCRACK IN FWD CARGO DOOR CROSSBEAM 1.25 INCH THROUGH FASTENER HOLE COMMON TO LWR TEE AND BEAM. INSTALLED FILLER AND REPAIR DOUBLER ON CROSSBEAM IAW AWA ER 03-5231-01130-DL1.May 30, 2001 · N168AW · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA0001787Bulkhead · crackedCRACK IN WEB BS 178 BLKHD WL 200 RBL 16.5. REPAIRED IAW SRM 53-10-08 PG 265-268, 216-220.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001786Skin · crackedR2 DOOR FUSELAGE LWR HINGE CUTOUT HFEC INDICATES CRACK BS 947.5 EMANATING FROM BENEATH WINDOW BELT DOUBLER .625 INCH AT WL 227. REPAIRED IAW SRM 53-60-01.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001785Frame · crackedLWR CHORD OF FWD CARGO DOOR CRACKED AT 3 FASTENER HOLES CONFIRMED BY HFEC. REPAIRED IAW AWA ER 03-5231-01130-DL1.May 30, 2001 · N168AW · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA0001784Web · crackedCOCKPIT LT FLOOR WEB CRACKED AT LIGHTENING HOLE BS 180 LBL 24 WL 207. REMOVED AND REPLACED FLOOR WEB IAW SRM 51-40-02 PG 2-3 AND 51-20-01 PG 1-6 & 10.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001783Bulkhead · crackedHFEC INDICATES CRACK BS 178 BLKHD WEB WL 199 LBL 4.7 FWD SIDE. REPAIRED IAW SRM 53-10-08 PG 287-298.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001782Bulkhead · crackedULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP LBL 4.7 WL 209.7-210. REPAIRED IAW SRM 53-10-08 PG 287-298.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001781Bulkhead · crackedULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP RBL 4.7 WL 212-212.6. REPAIRED IAW SRM 53-10-08 PG 287-298.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001780Bulkhead · crackedULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP RBL 4.7 WL 198.5-198.7. REPAIRED IAW SRM 53-10-08 PG 287-298.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001779Bulkhead · crackedULTRASONIC CRACK INDICATION BS 178 BLKHD WEB BENEATH STRAP FWD SIDE WL 218 RBL 14.1-13.3. REPAIRED IAW SRM 53-10-08 PG 265-268.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001778Strap · crackedFOUND BS 178 BLKHD FWD SIDE 0 BL STRAP CRACKED THROUGH WL 187. REPLACED STRAP IAW SRM 51-40-02 AND 51-20-01.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001777Web · crackedCOCKPIT RT FLOOR WEB CRACKED AT LIGHTENING HOLE BS 180 RBL 24 WL 207. REMOVED AND REPLACED WEB IAW SRM 51-40-02 PG 2-3, 10-11 AND 51-20-01 PG 1-6 & 10.May 30, 2001 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001775Bulkhead · crackedTEMPORARY CHERRY MAX INSTALLED REPAIR BS 178 BLKHD WEB WL 189 LBL 21. REPAIRED IAW SRM 53-10-08 PG 216-220 AND 51-40-02 PG 2-3, 10-11 AND 51-20-01 PG 1-6, 10.May 29, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001774Doubler · chafedRT WING OUTBOARD FOREFLAP OUTBOARD L/E REPAIR DOUBLER CHAFED 2 SPOTS. REMOVED DOUBLER IAW SRM 51-40-02 PG 9; TRIMMED OUT CRACKED AREA IAW SRM 57-53-01 PG 201-201; FORMED, DRILLED AND LOCATED IAW SRM 57-53-01 PG 202; TREATED AND PRIMED IAW SRM 51-20-01; INSTALMay 29, 2001 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA0001772Bulkhead · crackedAFT SIDE BLKHD WEB BS 178 CRACKED 2 PLACES LBL .6 WL 187.2-188.6 AND RBL .6 WL 187.1-188.6. REPAIRED IAW SRM 53-10-08 PG 287-298.May 29, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001771Frame · crackedFUSELAGE FRAME FITTING CRACKED AT FLOORBEAM ATTACH POINT RT SIDE BS 616. REMOVED FASTENER AND CUT OUT AREAS IAW AWA ER 03-5311-01157-KB1; FORMED ANGLE, FILLER IAW ER 03-5311-01127-KB1; DRILLED, TREATED AND PRIMED FILLER AND CAD PLATED ANGLE IAW ER 03-5311-011May 29, 2001 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001770Bulkhead · crackedAFT SIDE BS 178 BLKHD WEB CRACKS RBL .7-1.3 WL 205.7 AND LBL 1-1.5 WL 206. REPAIRED IAW SRM 53-10-08 PG 287-298.May 29, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001769Bulkhead · crackedCRACKED BS 178 BULKHEAD WEB WL 201.5 RBL 4.7. REPAIRED IAW SRM 53-10-08 PG 287-298.May 29, 2001 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001768Frame · crackedVERTICAL CHORD CRACKED BS 178 LBL 5.7 WL 184. REPAIRED AFT SIDE VERT CHORD IAW SRM 53-10-08 PG 221-235, 238-240.May 29, 2001 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001767Slat · crackedRIGHT WING NR 6 SLAT CRACKED AT FASTENER HOLE WBL 550 LOWER SURFACE. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01.May 29, 2001 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA0001766Slat · crackedNR 5 SLAT LOWER SURFACE CRACKED AT TWO FASTENER HOLES WBL 392. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01 PG 216-219.May 29, 2001 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA0001765Slat · crackedRIGHT WING NR 4 SLAT CRACKED AT 3 FASTENER HOLES AT WBL 253-257. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01.May 29, 2001 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AUS20010546Valve · failed(AUS) PRESSURISATION SYSTEM AUTOMATIC FLOW CONTROL VALVE FAILED TO CLOSE.May 23, 2001 · Boeing 73733A · Pressure Regulator/Outflow ValveSDR AWXA0001760Seat Track · corrodedFWD GALLEY SEAT TRACK BS 312 LBL 30 IS CORRODED. REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW TRACK IAW SRM 51-40-02 AND REF 53-00-52.May 16, 2001 · N166AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0001759Threshold · corrodedR2 DOOR THRESHOLD HAS CORROSION FROM STA 992 - 967 UNDERNEATH THRESHOLD. REMOVED AND REPLACED DOOR THRESHOLD INNER CHORD THAT WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-40-2.May 16, 2001 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001758Frame · crackedBS 178 BLKHD VERT CHORD AT LBL 5.7 HAS AN APPROX 2.5 INCH CRACK ON INBD FLANGE AT WL 181. REMOVED PARTS FOR ACCESS; CUT OUT DAMAGE; FABBED REPAIR PARTS, FILLERS, ANGLE AND STRAPS; INSTALLED, TREATED, PRIMED AND TOP COATED IAW SRM 51-30-01 AND 51-20-01 AND 53-May 16, 2001 · N166AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001755Pan · corrodedSURFACE CORROSION ON THE PLATE UNDER THE AFT LAV TANKS FWD FROM FWD FACE OF APB TO STA 1006. REMOVED AND INSTALLED NEW AFT FLOOR PANS IAW DWG 65-46812.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001754Pressure Panel · crackedA .75 INCH LONG CRACK COMING OUT OF FASTENER HEAD AT NLG BEAM WEB ADJACENT TO NLG WARNING HORN BRACKET MOUNT BS 225. REPAIRED IAW AWA ER 03-5310-01119-SS2.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA0001753Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 1006-1016 RBL 38. FABBED NEW FLOOR SUPPORT IAW SRM 53-60-51.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001752Bulkhead · crackedRHS INTERCOSTAL ATWL 207 HAS CRACK IN WEB AT BS 179.5 APPROX 1.25 INCH LONG. REMOVED DAMAGED WEB; FABBED AND INSTALLED NEW WEB IAW DWG 65-45833 AND SRM 51-40-2.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001751Stringer · crackedSTR 27L STA 967 CRACKED WHERE ATTACHED TO TIE CLIPC: REMOVED DMGD AREA OF STR; FABBED REPAIR PARTS; TREATED, PRIMED, TOPCOATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-03.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA0001750Intercostal · crackedINTERCOSTAL AT BS 178 BLKHD RHS AT WL 207 IS CRACKED. REPAIRED IAW AWA ER 03-5313-01119-BA1.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001749Bulkhead · crackedWEB AT WL 207 HAS CRACK IN WEB AT BS 179.5 APPROX .300 INCH LONG. REMOVED, FABBED AND REPLACED DAMAGED WEB IAW S/B 737-53A1173 AND DWG 45833.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001748Frame · corrodedCORROSION AND BULGED BETWEEN FRAME STRUCTURES AT INTERIOR BELLY OF FWD SIDE APB FRAME AND CIRCUM FRAME STA 1016 LBL 3 - RBL 3. REMOVED AND REPLACED STRINGER END FITTINGS AND FRAME T-CHORD SPLICE PNL IAW SRM 53-80-08 AND 51-40-2.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001747Floorbeam · corrodedFLOORBEAM AT STA 986.5 HAS SURFACE CORROSION. REPAIRED IAW AWA ER 03-5305-01117-DD3.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA0001746Skin · damagedFUSELAGE SKIN STA 187 WL 195 LBL 32 ELONGATED HOLE FOUND ON INTERCOSTAL REMOVAL. REPAIRED SKIN IAW SRM 53-00-01 FIG 201.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001745Stringer · corrodedCORROSION ON STR SIDES 27L AT STA 1006. BLENDED OUT CORROSION - FOUND OUT OF LIMITS; FABBED REPAIR PARTS; HEAT TREATED; TREATED AND PRIMED PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-00-03.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA0001744Floorbeam · corrodedCORROSION ON STA 1016 FLOORBEAM FROM LBL 12 - RBL 35. REPAIRED FLOORBEAM IAW AWA ER 03-5310-01118-JS1.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA0001743Bulkhead · corrodedCORROSION ON APB INTERIOR SKIN AND LAP SEAM STIFFENERS AFT STA 1016 BL 0 AND BELLY. REPAIRED APB SKIN IAW S/B 737-53A1075 AND DWG 65C28106 IAW AWA ER 03-5312-01120-ES1.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001742Floor Support · crackedAFT CARGO FLOOR SUPPORT Z-ANGLE RBL 20 STA 727-767 FOUND CRACKED DURING CORROSION REMOVAL. FABBED AND INSTALLED NEW FLOOR SUPPORT Z-ANGLE IAW SRM 53-60-53.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001741Seat Track · crackedCRACK APPROX 1 INCH ON SEAT TRACK T-EXTRUSION FLANGE EDGE TO FASTENER HOLE AT STA 727B LBL 45. REMOVED, FABBED AND INSTALLED NEW REPAIR STRAP IAW AWA ER 03-5310-01110-551.May 14, 2001 · N166AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0001740Crease Beam · corrodedLT CREASE BEAM CORRODED STA 967-1006. REMOVED AND REPLACED IAW SRM 53-40-02.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA0001739Frame · crackedBS 178 BLKHD VERT CHORD AT LBL 5.7 HAS CRACK APPROX 2.5 INCHES ON INBOARD FLANGE AT WL 181. CUT OUT DAMAGE; FABBED REPAIR PARTS; TREATED AND PRIMED; TOPCOATED AND INSTALLED IAW SRM 51-30-01, 51-20-01 AND 53-10-08.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001738Threshold · corrodedR2 DOOR THRESHOLD HAS CORROSION FROM STA 992-967 UNDERNEATH THRESHOLD. REMOVED AND REPLACED R2 DOOR THRESHOLD INNER CHORD THAT WAS FOUND OUT OF LIMITS IAW SRM 51-40-2.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001737Seat Track · corrodedFWD GALLEY SEAT TRACK BS 312 RBL 30 IS CORRODED. REMOVED DAMAGED SEAT TRACK SECTION AND REPLACED WITH NEW TRACK SECTION IAW SRM 51-40-02 AND 53-00-52.May 14, 2001 · N166AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0001736Floorbeam · corrodedSTA 1006 FLOORBEAM HAS CORROSION RBL 14-28. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 203.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA0001735Floorbeam · corrodedFLOORBEAM STA 967 HAS SURFACE CORROSION LBL 30-31. REMOVED CORROSION; FABBED AND INSTALLED REPAIR STRAP AND TAPERED FILTER IAW SRM 53-00-51.May 14, 2001 · N166AW · Boeing 73733A · Fuselage Main, Floor Beam
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