Boeing 737-244
Service difficulty reports · 176
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 = '737244' 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.
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 = '737244' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR P2EA01081Rib · chafedOKC - DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER BALANCE BAY RIB WEB CHAFED AT ES 66.54 ES 94.07, ES 121.59 AND 149.12. REPAIRED IAW DRAWING 55-01204-1 AND DETERMINED TO BE MAJOR ON 8110-3 DATED MAY 9, 2001. (M)SDR P2EA01043Angle · crackedOKC - DURING C-CHECK, L-ANGLE CRACKED AT BS 1150 WL 238, RIGHT SIDE. REPAIRED L-ANGLE IAW SRM 51-40-3. (M)SDR P2EA01067Strap · crackedOKC - DURING C-CHECK, INNER TEAR STRAP AT BS 1136 TO BS 1156 WL 240 ON RIGHT SIDE OF APU TORQUE BOX CRACKED 5 INCHES. FABRICATED TEAR STRAP AND REPLACED IAW SRM 51-20-1. (M)SDR P2EA01038Strap · crackedDURING C-CHECK, INNER TEAR STRAP AT BS 1136 TO BS 1156, WL 240 ON RIGHT SIDE IS CRACKED. (M)SDR P2EA001088Angle · corrodedOKC - DURING C-CHECK, FOUND CORROSION ON EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156. FOUND TO BE OUT OF LIMITS, LEVEL 2. REPAIRED EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156 IAW BOEING SRM 51-30-5, 51-20-1. (M)SDR P2EA01041Angle · corrodedOKC - DURING C-CHECK, FOUND CORROSION ON EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156. FOUND TO BE OUT OF LIMITS 5/1/2001. (M)SDR P2EA01065Frame · dentedOKC - DURING C-CHECK, FRAME AT BS 827 DENTED BETWEEN 24L AND 25L, LENGTH 2 INCHES, WIDTH 1 INCH, DEPTH .080 INCH. REPAIRED IAW SRM 53-10-4. (M)SDR P2EA01064Frame · crackedOKC - DURING C-CHECK, FLOOR UPPER CHORD AFT FLANGE AT BS 328 BL 0 CRACKED .400 INCHES. REPAIRED FLOORBEAM PER SRM 53-10-9. (M)SDR P2EA001082Beam · gougedOKC - DURING C-CHECK, FOUND THE RIGHT MLG SUPPORT BEAM GOUGED 10 INCHES INBOARD FROM THE LOWER OUTBOARD END, AFTER BLENDING IT WAS FOUND TO BE OUT OF LIMITS. REPAIRED THE RT MLG SUPPORT BEAM GOUGED 10 INCHES INBOARD FROM THE LOWER OUTBOARD END PER BOEING TELESDR P2EA001085Skin · corrodedOKC - DURING C-CHECK, FOUND THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R, LEVEL 2. REPAIRED THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R IAW BOEINGSDR P2EA001017Beam · gougedOKC - DURING C-CHECK, FOUND THE RIGHT MAIN LANDING GEAR SUPPORT BEAM GOUGED 10 INCHES INBAORD FROM THE LOWER OUTBOARD END. AFTER BLENDING IT WAS FOUND TO BOUT OF LIMITS. (M)SDR P2EA001018Skin · corrodedOKC - DURING C-CHECK, FOUND THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R. (M)SDR P2EA001032Skin · crackedOKC - DURING C-CHECK, FOUND THE FORWARD FUSELAGE SKIN T STATION 196.5 AT LBL 3 WITH CRACK, .75 INCH IN LENGTH. REPAIRED THE FORWARD FUSELAGE SKIN AT STATION 196.5 TAT LBL 3.0 IAW BOEING SRM 53-30-3 FIG 1. (M)SDR P2EA001015Skin · crackedOKC - FOUND DURING C-CHECK, FORWARD FUSELAGE SKIN AT STATION 196.5 TO 203.5 AT LBL 3 WITH CRACK .75 INCH IN LENGTH. (M)SDR P2EA001016Skin · corrodedOKC - DURING C-CHECK, FOUND THE INTERNAL SKIN AT FUSELAGE STATION 322 BETWEEN STRINGERS 28-29 RIGHT HAS CORROSION. (M)SDR P2EA001083Landing Gear · wornOKC - DURING C-CHECK, FOUND THE RIGHT MAIN LANDING GEAR TRUNNION RACE WITH WEAR OUT OF LIMITS. REPAIRED THE RIGHT MLG TRUNNION RACE IAW BOEING OVERHAUL MANUAL, SEE FAA FORM 8130-3 TRACKING NR W/O 323910 FROM REPAIR STATION VQ4R605M. (M)SDR P2EA001084Skin · crackedOKC - DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUB CUTOUT WITH CRACK, .25 INCH. REPAIRED THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUBE CUTOUT IAW BOEING SRM 57-30-4 FIG 1. (M)SDR P2EA001014Skin · crackedOKC - DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUB CUTOUT WITH CRACK, LENGTH .25 INCH. (M)SDR P2EA01080Rib · chafedOKC - DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER BALANCE BAY RIB WEBS CHAFED AT ES 66.54, ES 94.07 ES 121.59 AND ES 149.12. REPAIRED IAW DRAWING 55-01204-1 AND DETERMINED TO BE MAJOR ON 8110-3 DATED MAY 9, 2001. (M)SDR P2EA001031Skin · corrodedOKC - DURING C-CHECK, FOUND THE LEFT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE LEFT RAM AIR DUCT WITH CORROSION OUT OF LIMITS AT LBL 41, STRINGER 5C. REMOVED CORROSION AND TREATED. (M)SDR P2EA001030Skin · corrodedOKC - DURING C-CHECK, FOUND THE RIGHT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE RIGHT RAM AIR DUCT WITH CORROSION OUT OF LIMITS AT RBL 40.5 THROUGH 43.5, STRINGER 4C AND 5C. REMOVED CORROSION AND TREATED. (M)SDR P2EA001013Skin · corrodedOKC - DURING C-CHECK, FOUND THE LEFT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE LEFT RAM AIR DUCT WITH CORROSION OUT OF LIMITS. (M)SDR P2EA01053Flap · delaminatedOKC - DURING C-CHECK, RIGHT WING INBOARD MID-FLAP OUTBOARD EDGE DELAMINATED 6.5 INCHES, WIDTH 1 INCH. REPAIRED IAW SRM 51-40-20. (M)SDR AALA01037Flap · delaminatedOKC - DURING C-CHECK, LEFT WING OUTBOARD MID-FLAP INBOARD EDGE DELAMINATED, LENGTH 2 INCHES, WIDTH 1 INCH. REPAIRED IAW SRM 57-50-2 AND SRM 51-40-2. (M)SDR P2EA001009Skin · delaminatedOKC - DURING C-CHECK, FOUND THE LEFT WING OUTBOARD MID-FLAP INBAORD EDGE WITH DELAMINATION, LENGTH 2 INCHES, WIDTH 1 INCH. (M)SDR P2EA001068Skin · delaminatedDURING C-CHECK, FOUND THE RIGHT WING INBOARD MID-FLAP OUTBOARD EDGE WITH DELAMINATION, LENGTH 6.5 INCH, WIDTH 1 INCH. (M)SDR P2EA01049Floorbeam · corrodedOKC - DURING C-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 312, BOTTOM AFT SIDE OF UPPER CHORD AT BL 0, LBL 8 AND RBL 8. REPAIRED PER DRAWING 53-01181-1 AND 8110-3. (M)SDR P2EA001012Skin · corrodedOKC - DURING C-CHECK, FOUND THE RIGHT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE RIGHT RAM AIR DUCT WITH CORROSION OUT OF LIMITS. (M)SDR P2EA01004Seal · failedMCI - FLT 350 - WHILE IN CLIMB-OUT OF MCI, AIRCRAFT WOULD NOT PRESSURIZE, RETURN TO MCI. INSPECTION FOUND AIRCRAFT L1 DOOR SEAL NOT PROPERLY SEATED. RESECURED DOOR AND OPERATIONAL CHECK NORMAL. (M)SDR P2EA00463Lever · malfunctionedMSY - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO MSY WITH NO INCIDENT. RESET LANDING GEAR LEVER AND PRESSURE WARNING CIRCUIT BREAKERS, SYSTEM CHECKED NORMAL PER MM 32-31-0. (M)SDR P2EA00274Floorbeam · corrodedSJO - FOUND DURING C-CHECK, CORROSION ON FLOORBEAM LOWER CHORD AT BS 867, RBL 25 AND WL 202. REPAIRED FLOORBEAM LOWER CHORD AT BS 867 WL 202 BETWEEN RBL 16 AND RBL 36 IAW SRM 53-10-9 FIG 7. (M)SDR P2EA00273Bulkhead · damagedSJO - DURING C-CHECK, TEMPORARY REPAIR AT BS 178 FROM LBL 8 TO LBL 15 AND FROM WL 233 AND WL 238. INSTALLED PERMANENT REPAIR AT BS 178 FROM LBL 8 TO LBL 15 AND FROM WL 233 TO WL 238 IAW SRM 53-10-1 FIG 1. (M)SDR P2EA00272Skin · damagedSJO - DURING C-CHECK, RIGHT FORWARD AND AFT CORNERS WORN ON E/E DOOR. REPAIRED RIGHT SKIN SECTIONS AT FORWARD AND AFT CORNERS IAW SRM 52-00-3 FIG 5. (M)SDR P2EA00263Bulkhead · crackedSJO - DURING C-CHECK, TEMPORARY REPAIR AT BS 178 FROM RBL 8 TO RBL 15 AND BETWEEN WL 233 TO WL 238. INSTALLED PERMANENT REPAIR AT BS 178 FROM RBL TO RBL 15 AND FROM WL 233 TO WL 238 IAW SRM 53-10-11 FIG 1. (M)SDR P2EA00285Rudder · delaminatedSJO - DURING C-CHECK, RUDDER DELAMINATION BETWEEN STA 17.25 AND STA 35.25. REPAIRED RUDDER IAW SRM 51-40-9, PARAGRAPH 3 AND PARAGRAPH 5, FIG 3. (X)SDR P2EA00282Web · corrodedDURING C-CHECK, CORROSION (LEVEL 2) ON WEB SECTION AT BS 178 FROM LBL 16 TO LBL 29 AND BETWEEN WL 180 AND WL 240. REPAIRED WEB SECTION AT BS 178 FROM LBL 16 TO LBL 29 AND BETWEEN WL 180 AND WL 240 IAW SRM 51-10-1 PAGE 8, PARA 6. (X)SDR P2EA00281Skin · delaminatedSJO - DURING C-CHECK, LEFT WING NR 1 SPOILER UPPER SKIN WITH DELAMINATION. REPAIRED NR 1 SPOILER IAW COOPESA EO COO-CMP-3-57-609-00, DATED OCT 2, 2000. (M)SDR P2EA00280Skin · delaminatedSJO - FOUND DURING C-CHECK, LEFT OUTBOARD FLIPPER FLAP UPPER AND LOWER SKIN WITH DELAMINATION. REPAIRED FLIPPER FLAP SKIN IAW COOPESA EO COO-CMP-3-57-607-00 DATED SEPT 29, 2000. (M)SDR P2EA00276Skin · delaminatedSJO - FOUND DURING C-CHECK, LEFT WING SPAR LOWER ACCESS PANEL INNER SKIN DELAMINTATED FROM RSS 339 TO 380. REPAIRED PANEL IAW COOPESA EO COO-CMP-3-57-608-00, DATED 9/29/2000. (M)SDR P2EA00260Skin · crackedSJO - DURING C-CHECK, LFEC SKIN CRACK INDICATION BETWEEN BS 755 AND BS 760 AT STRINGER 25R. REPAIRED SKIN FROM BS 755 TO BS 769 BETWEEN STRINGERS 24R AND 26R IAW SRM 53-30-3 FIG 13 DETAIL II. (M)SDR P2EA00259Skin · crackedSJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION AT BS 366 STRINGER 19R. REPAIRED SKIN FROM BS 306 TO BS 371 BETWEEN STRINGERS 18R AND 20R IAW SRM 53-30-3 FIG 13 DETAIL I. (M)SDR P2EA00258Skin · crackedSJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION AT BS 778 STRINGER 25L. REPAIRED SKIN FROM BS 751 TO BS 795 AND BETWEEN STRINGERS 24L AND 26L IAW SRM 53-30-3 FIG 13 DETAIL II. (M)SDR P2EA00271Skin · crackedSJO - DURING C-CHECK, MFEC SKIN CRACK ON LOWER ROW OF FASTENERS AT BS 877 STRINGER 25R. REPAIRED SKIN FROM BS 870 TO BS 883 AND FROM STRINGERS 25R TO 27R IAW SRM 53-30-3 FIG 13 DETAIL II. (M)SDR P2EA00270Skin · crackedSJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION ON LOWER ROW OF FASTENERS AT BS 1006 STRINGER 4L. REPAIRED SKIN FROM BS 1000 TO BS 1012 AND BETWEEN STRINGER 3L AND 5L IAW SRM 53-30-3 FIG 13 DETAIL II. (M)SDR P2EA00269Skin · crackedSJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION, 2 INCHES LONG, ON UPPER ROW OF FASTENERS AT STRINGER 26L BETWEEN FROM BS 460 TO BS 464. REPAIRED SKIN FROM BS 455 TO BS 466 AND FROM STRINGERS 25L TO 27L IAW SRM 53-30-3 FIG 13 DETAIL II. (M)SDR P2EA00279Skin · crackedSJO - DURING C-CHECK, FOUND MFEC SKIN CRACKED INDICATIONS 3 INCHES LONG FROM BS 515 TO 518 AT STRINGER 10R. REPAIRED SKIN FROM BS 510 TO BS 500A PLUS 1 AND BETWEEN STRINGERS 9R TO 11R IAW SRM 53-30-3 FIG 13. (M)SDR P2EA00284Bulkhead · crackedSJO - DURING C-CHECK, VERTICAL CHORD CRACKED AT BS 178. LBL 5.7 AND WL 184. FABRICATED AND REPLACED VERTICAL CHORD AT BS 178, LBL 5.7 AND FROM WL 177 AND WL 197 IAW SRM 53-10-11 FIG 8 AND SRM 51-10-1. (X)SDR P2EA00262Skin · crackedSJO - DURING C-CHECK, SIX SKIN CRACKS, AVERAGE LENGTH .25 INCH, AT BS 188, WL 214, TWO BS 188 WL 216, ONE AT BS 203, WL 216, ONE AT BS 211, WL 217 AND TWO AT BS 211 WL 218 ON RT SIDE OF AIRCRAFT. REPAIRED RIGHT SKIN CRACKS FROM BS 183 TO BS 244 AND FROM WL 20SDR P2EA00278Skin · debondedSJO - DURING C-CHECK, UPPER WINDOW BELT DISBONDING FROM BS 360 TO BS 380 AND BETWEEN STRINGER 11R AND 13R. REPAIRED WINDOW BELT FROM BS 360 TO BS 380 AND FROM STRINGER 10R TO 14R IAW SB 737-53-1078, SECTION III, PART III PARAGRAPH C, FIG 3 AND FIG 6 DATED SEPSDR P2EA00277Skin · debondedSJO - DURING C-CHECK, UPPER WINDOW BELT DISBONDING FROM BS 887 TO BS 907 AND BETWEEN STRINGER 11L AND 13L. REPAIRED WINDOW BELT FROM BS 887 TO BS 907 AND BETWEEN STRINGER 10L AND 14L IAW SB 737-53-1078, SECTION III, PART III, PARAGRAPH C, FIG 3 AND FIG 6 DATE
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