Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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 = '727224' 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 CALA9900840Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN RT LOWER FUSELAGE SKIN AT STA 680, STRINGER 28R. THE CRACKED AREA AND FASTENERS WERE REMOVED IAW SRM 51-30-2, PAGE 2 AND 53-30-3, PAGE 14E. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-30-3, PAGE 14E.SDR CALA9900839Web · crackedINSPECTION FOUND TWO CRACKED WEBS AT FORWARD CARGO COMPARTMENT DOOR AFT EDGE. THE CRACKS WERE .5 INCH LONG. NEW WEBS WERE INSTALLED IAW SRM 52-30-1 AND 51-30-2.SDR CALA9900712Switch · inoperativeTHE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING IAH. GEAR RECYCLING DID NOT HELP. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. BOTH NOSE GEAR DOOR SWITCHES WERE REMOVED AND REPLACED IAWSDR CALA9900672Battery Pack · dischargedINSPECTION FOUND THE RT AFT OVERWING EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW MM 33-50-01.SDR CALA9900656Power Pack · inoperativeINSPECTION FOUND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE POWER PACK ASSEMBLY WAS REPLACED AND OPERATION CHECKED GOOD.SDR CALA9900657Battery · dischargedINSPECTION FOUND BOTH FORWARD ENTRY EMERGENCY FLASHLIGHTS WITH CHARGE LIGHTS NOT BLINKING. THE BATTERIES FOR BOTH FLASHLIGHTS WERE REMOVED AND REPLACED IAW MM 25-60-00.SDR CALA9900653Keel Beam · crackedINSPECTION FOUND A 4 INCH CRACK IN KEEL BEAM CHORD AT STA 950E, STRINGER 29R. A REPAIR WAS INSTALLED IAW ECRA 5310-03862.SDR CALA9900652Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AROUND BELLY DRAIN AT STA 950E BETWEEN STRINGER 29R TO 30. A REPAIR WAS INSTALLED IAW ECRA 5330-02822.SDR CALA9900651Floorbeam · corrodedINSPECTION FOUND MAIN CABIN FLOORBEAM CAP CORRODED AT STA 1130 FROM RBL 25-45. THE FLOORBEAM CAP WAS REMOVED AND REPLACED IAW ECRA 5310-03861.SDR CALA9900632Wire · brokenTHE EMERGENCY PATH LIGHTING AT SEAT NR 12 WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOUND AT LIGHT ASSEMBLY AND OPERATION CHECKED GOOD IAW MM 33-50-02, PAGE 201.SDR CALA9900614Angle · crackedINSPECTION FOUND A .3125 INCH CRACK IN DOUBLER ANGLE AT RT WING FRONT SPAR WBL 92. THE ANGLE AND STIFFENER WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, FIGURE 4.SDR CALA9900637Battery Pack · dischargedINSPECTION FOUND R-2 DOOR UPPER EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.SDR CALA9900636Battery Pack · dischargedINSPECTION FOUND L-1 DOOR UPPER EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.SDR CALA9900635Battery Pack · dischargedINSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.SDR CALA9900634Battery Pack · dischargedINSPECTION FOUND LT AFT EXTERNAL EMERGENCY LIGHT ON AFT WING FAIRING WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW MM 33-50-01, PAGE 501.SDR CALA9900608Skin · delaminatedINSPECTION FOUND NR 1 SPOILER PANEL UPPER SKIN DELAMINATED. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-61-81.SDR CALA9900566Stringer · corrodedINSPECTION FOUND STRINGER 27R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 620. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A STRINGER REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-6.SDR CALA9900565Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 FROM RBL 25-45. A REPAIR WAS INSTALLED IAW SRM 51-10-8, PAGE 18.SDR CALA9900558Flap · crackedINSPECTION FOUND A .125 INCH CRACK WITH DENT IN THE RIGHT I/B MIDFLAP TRAILING EDGE INBOARD MOST END. THE FLAP WAS REPAIRED IAW SRM 51-40-6.SDR CALA9900557Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO FRAME AT STA 620, RBL 27-28. THE CRACKED AREA WAS CUT OUT, A SPLICE REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-10-6 AND 51-30-2.SDR CALA9900556Support · corrodedINSPECTION FOUND FLOOR SUPPORT J-ANGLE CORRODED AROUND SCREW HOLES AT BS 1070 BETWEEN RBL 45 AND 62. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, PAGE 1 AND 51-20-2, PAGE 1.SDR CALA9900549Skin · debondedINSPECTION FOUND LEFT I/B FOREFLAP UPPER SKIN DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.SDR CALA9900548Angle · corrodedINSPECTION FOUND CABIN FLOOR CHORD ANGLE AT STA 1178, RBL 46 CORRODED AROUND LAV TANK AFT I/B MOUNT BOLT. THE CORRODED AREA WAS REMOVED AND A REINFORCEMENT CHORD REPAIR WAS INSTALLED IAW ECRA 5310-01585.SDR CALA9900547Support · corrodedINSPECTION FOUND CABIN FLOOR PANEL SUPPORT CORRODED AT STA 1035, RBL 15 TO RBL 62. THE CORROSION WAS REMOVED IAW SRM 51-6-1. THE SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 1 AND 51-10-1, PAGE 4.SDR CALA9900546Skin · gougedINSPECTION FOUND RT WING I/B FOREFLAP BULLNOSE LOWER SIDE ABOVE CENTER HINGE POINT GOUGED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-50-00.SDR CALA9900542Web · chafedAFT AIR STAIR ENTRY WAY LEFT WEB PANEL HAS CHAFE MARKS (6 EA) FROM STA 1283 TO 1342. FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER SRM 52-01 FIG 61, 51-10-2, AND 51-30-2.SDR CALA9900539Skin · debondRIGHT INBOARD AFT FLAP AFT SEGMENT UPPER SURFACE HAS 3.25 CHAFED SPOT AND 1.25 X .75 DEBOND AREA 27.5 FROM INBOARD END. REMOVED AND REPLACED FLAP.SDR CALA9900522Intercostal · corrodedSTATION 700 TO 720 STRINGER 28R OUTBOARD INTERCOSTAL FLANGE CORRODED. CUT OUT DAMAGED AREA. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-3, 51-10-6 AND 51-30-2.SDR CALA9900521Skin · gougedUPPER RUDDER TRAILING EDGE JUST BELOW NR 2 CONTROL TAB ATTACH HINGE (FROM BOTTOM) AREA GOUGED. REMOVED DAMAGED AREA BY ROUTING, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 51-10-2 AND 51-40-2.SDR CALA9900520Mechanism · hung upAFT ENTRY DOOR DOES NOT OPEN SMOOTHLY, HANGS UP AT BOTTOM. ADJUSTED AFT DOOR UPPER LATCH FITTING PER MM 52-13-0 PAGE 405.SDR CALA9900519Stringer · corrodedCORROSION AT STA 28R INBOARD BETWEEN STATION 700 AND 720. REMOVED FAIRING RIBS STA 700 TO 710 RIGHT. CUT OUT DAMAGED AREA, REMOVED INTERCOSTAL STA 700 TO 720 STR 28 RIGHT. ACCOMPLISHED HFEC, NO CKACK FOUND. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIRSDR CALA9900518Floorbeam · corrodedFLOORBEAM FS 312 HAS 2 HOLES WITH CORROSION AT LBL 20 AND 3. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 53-10-9 FIG 8.SDR CALA9900517Web · corrodedFLOOR LEVEL WEB CORRODED WHERE FS 1178 CHORD ANGLE REMOVED AT RBL 34. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED PER SRM 53-41-2.SDR CALA9900516Chord · crackedAPPROX 2.25 INCH CRACK BELOW OUTBOARD UP STOP PAD AT LOWER CHORD RIGHT WING NR 8 SLAT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-4, 51-10-2 AND 51-30-2.SDR CALA9900515Skin · bulgedFUSELAGE LOWER SKIN BETWEEN STATIONS 1050 TO 1070 AND STRINGER 30 AREA BULGED. REMOVED FASTENERS FROM FUSELAGE SKIN, NO CORROSION WAS FOUND. FABRICATED DOUBLER USING 2024 T3 .080 TREATED, PRIMED AND INSTALLED PER SRM 51-30-2 AND 53-30-3.SDR CALA9900514Channel · crackedRIGHT ELEVATOR LOWER SKIN FORWARD OF CONTROL TAB INNER CHANNEL CRACKED (.5). STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 55-20-3, 51-10-1 AND 51-30-2.SDR CALA9900513Beam · corrodedCABIN STA 328 TO 344 LBL 30 J BEAM CORRODED. REMOVED J BEAM, RECEIVED EXTRUSION, DRILLED, TREATED, PRIMED AND INSTALLED PER SRM 51-30-2.SDR CALA9900512Intercostal · corrodedINTERCOSTAL CORROSION FS 400 TO 420 RBL 12. REMOVED INTERCOSTAL, FABRICATED, TREATED, PRIMED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-6, 51-10-1, 51-10-2 AND 51-30-2.SDR CALA9900511Skin · crackedRIGHT ELEVATOR LOWER SKIN JUST FORWARD OF CONTROL TAB AREA CRACKED (3). STOP DRILLED CRACK. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-10-1, AND 55-20-3.SDR CALA9900510Intercostal · crackedINTERCOSTAL CRACK AT 3 EACH TOP FLANGE HOLES BETWEEN FLOORBEAMS 760 TO 740 0 BL (1). REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED PER SRM 51-10-2 AND 51-30-2.SDR CALA9900508Chord · corrodedCHORD CORROSION INBOARD OF LEFT CUTOUT AT FS 306 TO 348. REMOVED OLD ANGLE, FABRICATED, TREATED, PRIMED AND INSTALLED NEW ANGLE PER SRM 51-10-1.SDR CALA9900507Stringer · crackedVERTICAL STABILIZER INNER COMPARTMENT NR 8 RIB RT STRINGER NR 8 CRACKED AT ATTACH BOLT (2). STOP DRILLED CRACK, FABRICATED ANGLE AND FILLER REPAIR, TREATED AND PRIMED REPAIR PARTS, INSTALLED PER SRM 55-30-4, 55-30-9 AND 51-30-2.SDR CALA9900506Floorbeam · corrodedFLOORBEAM FS 344 HAS CORROSION TOP FLANGE BOTH SIDES RBL 24 TO LBL 60. REPAIRED AREA PER SRM 53-40-8 PAGE 51.SDR CALA9900505Shield Plate · crackedVERTICAL STABILIZER INNER COMPARTMENT SHIELD PLATE AT I/B 1 AND LEFT HAND STRINGER NR 7 AREA HAS A SMALL CRACK (.25). REMOVED FASTENERS, FABRICATED ANGLE PER SRM 55-30-6. TREATED, PRIMED AND INSTALLED DOUBLER PER SRM 51-10-2 AND 55-30-6 PG 2A.SDR CALA9900486Skin · chafedLEFT WING NR 4 SLAT LOWER TRAILING EDGE UPPER SURFACE CHAFED INBOARD TO OUTBOARD END. BURNISHED AREA. FOUND OUT OF LIMITS. FABRICATED, TREATED, PRIMED, AND INSTALLED DOUBLER PER SRM 57-50-3 PABE 2B.SDR CALA9900485Rib · crackedRIGHT OUTBOARD MID FLAP HAS .5 CRACK AT INBOARD MOST RIB LOWER END. INSTALLED DOUBLER AT RIB LOWER END OF MID FLAP PER SRM 51-40-3.SDR CALA9900483Floorbeam · corrodedFLOORBEAM CORRODED AT SCREW HOLE FS 400 RBL 35. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS, PICKED UP HOLES, TREATED, PRIMED, AND INSTALLED REPAIR PER SRM 51-10-6 AND 53-10-8 FIG 8.SDR CALA9900482Spar · crackedVERTICAL STAB UPPER RIGHT LEADING EDGE SPAR CRACKED (.25) AROUND RIVET AT STIFFENER PLATE JUST BELOW TENSION TIE FORWARD ATTACH BOLT. REMOVED FASTENERS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 55-30-6 AND 51-1-20.SDR CALA9900481Doubler · chafedLEFT OUTBOARD FLAP AFT SEGMENT UPPER L/E HAS CHAFED AREA AT DOUBLER 24 FROM OUTBOARD END. REMOVED PREVIOUS REPAIR. FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR PER SRM 57-50-4, 51-10-2, 57-51-4, AND 51-30-2.SDR CALA9900480Mount · crackedOUTBOARD BRACKET HAS .25 VISIBLE CRACK AT LOWER CORNER WHERE NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. REPAIRED BRACKET PER SRM 51-30-2 AND 51-20-1.
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