N27783, cancelled Apr 24, 2003
Service difficulty reports · 70
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 = 'N27783' AND deregistration_id = 'N27783-2003-04-24' 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 n_number = 'N27783' AND deregistration_id = 'N27783-2003-04-24' 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 CALA9900699Skin · corrodedINSPECTION FOUND FUSELAGE SKIN BULGED AFT OF EXTERNAL POWER RECEPTACLE AT STA 294, WL 160. THE BULGED AREA WAS CUT OUT. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3.SDR CALA9900693Skin · bulgedINSPECTION FOUND RT FUSELAGE BELLY SKIN BULGED AT FS 360 AFT OF MLG. A REPAIR WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.SDR CALA9900692Wire · brokenINSPECTION FOUND EMERGENCY PATH LIGHTING AT SEAT ROW 28 INOPERATIVE. WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.SDR CALA9900691Wire · brokenINSPECTION FOUND EMERGENCY PATH LIGHTING AT ROW 19 AND 20 INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.SDR CALA9900690Battery Pack · dischargedINSPECTION FOUND THE LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-00.SDR CALA9900689Battery Pack · dischargedINSPECTION FOUND MAIN CABIN EXIT LIGHT AT OVERWING EXIT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.SDR CALA9900688Battery Pack · dischargedINSPECTION FOUND LT CENTER OVERWING EMERGENCY EXIT LIGHT FLASHING. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.SDR CALA9900687Battery Pack · dischargedINSPECTION FOUND THE R-2 DOOR EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.SDR CALA9900580Connector · failedTHE RT MLG RED UNSAFE LIGHT ILLUMINATED STEADILY AT FIRST, AND THEN FLASHED ON AND OFF INTERMITTENTLY WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE TARGETS, SENSORS, AND WIRING WERE VISUALLY INSPECTED AND CHECKED GOOD. SDR CALA9802079Skin · dentedINSPECTION FOUND LT I/B TE FOREFLAP DENTED AND A 1 X 1 AREA OF DEBONDING JUST OUTBOARD OF NR 3 FLAP TRACK AREA AT LOWER SURFACE. THE LT I/B TE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.SDR CALA9802076Cover · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER T/E HINGE COVER OF NR 3 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-20-1 AND 51-30-2, PARAGRAPH 7.SDR CALA9802075Cover · crackedINSPECTION FOUND A .1875 AND .125 CRACK IN LT WING UPPER T/E HINGE COVER OF NR 2 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-30-2, PARAGRAPH 7.SDR CALA9802074Web · puncturedINSPECTION FOUND A PUNCTURE IN FORWARD CARGO AREA WEB JUST FORWARD OF UPPER AFT DOOR STOP. THE PUNCTURED AREA WAS ROUTED OUT IAW SRM 51-10-1, PAGE 6B. A WEB REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-10-2, PAGE 4.SDR CALA9802073Bracket · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN NR 6 LE FLAP O/B ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-20-1, FIGURE 18.SDR CALA9802072Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING NR 2 SLAT LOWER CHORD ANGLE BELOW TELESCOPING ANTI-ICE DUCT AREA. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, PAGE 16.SDR CALA9802071Plate · crackedINSPECTION FOUND A 1 INCH CRACK IN PLATE AT RT INBOARD MIDFLAP ABOVE AFT END OF NR 5 SPINDLE. THE PLATE WAS REMOVED IAW SRM 51-30-2, PAGE 4. A NEW PLATE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2, PAGE 1.SDR CALA9802070Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT SCREW HOLE TO RIVET HOLES OF NR 2 SLAT UPPER TRAILING EDGE WHERE I/B HOOK MOUNTS. THE FASTENERS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 3 AND 57-50-3, PAGES 27-28.SDR CALA9802069Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN SKIN AT AFT FACE OF LT WING NR 1 SLAT, INBOARD OF INBOARD TRACK AREA. THE NR 1 LE SLAT WAS REMOVED AND REPLACED IAW MM 27-81-11.SDR CALA9701801Accessory Unit · inoperativeTHE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT IAW MM 32-09-121. OPERATION OF THE GEAR CHECKED GOOD.SDR CALA9701436Light · inoperativeAFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS INOP. REPLACED LIGHT ASSEMBLY.SDR CALA9701036Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 480 FROM RBL 46 TO SIDEWALL. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3.SDR CALA9700961Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 720F, BL 0. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700960Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN WEB BELOW CABIN FLOOR TRACK AREA AT BS 885, RBL 45. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700959Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 277, RBL 12. A REPAIR WAS INSTALLED IAW SRM 51-10-1.SDR CALA9701035Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 BETWEEN RBL 25 AND RBL 46. THE CORROSION WAS REMOVED. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701034Floorbeam · corrodedINSPECTION FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 344, LBL 30. THE CORRODED SECTION WAS CUT OUT. A BEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700958Floor Track · corrodedINSPECTION FOUND FLOOR TRACK CORRODED AT BS 400 TO 440, RBL 46. THE FLOOR TRACK WAS REMOVED, A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9700957Floor Track · corrodedINSPECTION FOUND FLOOR TRACK CORRODED AT STA 1110 RBL 25. THE TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9700947Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 8 AND STRINGER 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.SDR CALA9700946Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 2 AND STRINGER NR 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.SDR CALA9701039Skin · crackedINSPECTION FOUND THREE 1 CRACKS AT LT WHEEL WELL KEEL BEAM SKIN AT FORWARD END OF APU CUTOUT, JUST AFT OF BS 870. THE CRACKED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND ECRA 5310-03522.SDR CALA9701037Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN MID UPPER AFT LT WING STRINGER AT RIB STATION 629. THE CRACK WAS STOP DRILLED. THE STRINGER WAS REPAIRED IAW BOEING SERVICE BULLETIN 57A159.SDR CALA9700962Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING STRINGER JUST FORWARD OF FUEL DUMP LINE AT STA 656.50. A REPAIR WAS FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-57A159.SDR CALA9700951Stringer · corrodedINSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED AT STA 720E. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A STRINGER AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.SDR CALA9700949Floorbeam · crackedINSPECTION FOUND A .5 INCH CRACK COMING FROM LIGHTENING HOLE IN FLOORBEAM AT BS 825, LBL 54. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700948Floorbeam · crackedINSPECTION FOUND A .5 AND .3125 INCH CRACK OUT OF LIGHTENING HOLE OF FLOORBEAM AT BS 825, RBL 49. THE CRACK WAS STOP DRILLED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700956Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 720A BETWEEN STRINGER 27R AND 28R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9701032Skin · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT SKIN BETWEEN STRINGER 27 AND 28 AT STA 720D CORRODED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700963Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 424, RBL 45. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9700955Stringer · corrodedINSPECTION FOUND STRINGER S28R IN FORWARD CARGO COMPARTMENT CORRODED AT STA 620. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 1.SDR CALA9700954Clip · crackedINSPECTION FOUND A .5 INCH CRACK IN S28L TIE CLIP AND A .5 INCH CRACK IN S28R TIE CLIP AT STA 460. REPLACEMENT TIE CLIPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-30-2, AND 51-10-3.SDR CALA9701038Spar · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING FRONT SPAR UPPER CHORD AT STA 335. THE CRACKED SECTION WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5710-01819 AND SRM 57-10-6.SDR CALA9701033Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT BOTTOM OF WINDOW POST AREA BETWEEN FIRST OFFICER'S WINDSHIELD AND SLIDING WINDOW. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 8.SDR CALA9701031Skin · dentedINSPECTION FOUND A DENT IN RT FUSELAGE SKIN AT STA 1086 TO 1093 BETWEEN STRINGER 21R AND 22R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9701030Bulkhead · crackedINSPECTION FOUND A 2.5 INCH CRACK IN BULKHEAD AT APU LOAD CONTROL CUTOUT, BS 870. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01544.SDR CALA9700953Skin · crackedINSPECTION FOUND A .1875 INCH CRACK IN FUSELAGE SKIN WITH CORROSION AT LAP SEAM BS 600, STRINGER 26L. THE CORROSION WAS REMOVED AND THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700952Skin · crackedINSPECTION FOUND .0625 INCH CRACKS AROUND RIVET HEADS OF FUSELAGE SKIN AT LAP SEAM 26L BETWEEN BS 575 TO 588. THE CRACKED AREA OF SKIN WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700950Skin · corrodedINSPECTION FOUND FUSELAGE SKIN BULGING WITH TWO FASTENERS POPPED AT LEFT LAP SEAM 26L BETWEEN BS 700 TO 715. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700672Lg Accy Unit · inoperativeTHE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN LANDING GEAR WAS EXTENDED ON APPROACH. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT AND OPERASDR CALA9601703Duct · brokenTHE NR 3 FIRE LIGHT AND BELL ACTIVATED IN FLIGHT. THE ENGINE THROTTLE WAS REDUCED TO IDLE AND THE WARNING CEASED. WHEN THE THROTTLE WAS INCREASED THE LIGHT CAME ON AGAIN. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND
Back to N27783, cancelled Apr 24, 2003