Boeing 727-223
Service difficulty reports · 5,313
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 = '727223' 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 = '727223' 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 ABXR200910030028Skin · gougedDURING A HEAVY MX INSP, THE MAIN CARGO DOOR CUT OUT AFT WEB WAS FOUND NICKED AND GOUGED OUT OF LIMITS. THE AFT WEB WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200910030027Stringer Splice · corrodedDURING A HEAVY MX INSP, A STRINGER SPLICE WAS FOUND CORRODED OUT OF LIMITS. FABRICATED NEW SPLICE FROM 7070-T6 0.070". TREATED, PRIMED AND REPLACED SPLICE. ITEM RETURNED TO SERVICESDR ABXR200910030029Skin · corrodedDURING A HEAVY MX INSP, THE LWR WING PLATE WAS FOUND EXFOLIATED ABOVE THE LT PRIMARY HEAT EXCHANGER. DAMAGED AREA APPROX 6" X 5", REMOVED ALL CORROSION, BEYOND MFG LIMITS. MACHINED PAD-UPS TO ACCOMMODATE EXTERNAL DOUBLER. SPOT FACED SANDWICHED FASTENER HEADS SDR ABXR200910030026Retainer · crackedDURING A HEAVY MX INSP, THE RT MLG BEAM SWING LINK LOWER PIN RETAINER WAS FOUND CRACKED. REMOVED AND REPLACED RT MLG DEAM SIWNG LINK LOWER PIN RETAINER. ITEM RETURNED TO SERVICESDR ABXR200910020025Skin · crackedDURING A HEAVY MX INSP EVENT, MAIN ENTRY DOOR INNER AFT EDGE BY MID DOOR STOPS WAS DISCOVERED CRACKED. INNER SKIN WAS REPAIRED AND ITEM RETURNED TO SERVICE.SDR ABXR200910020024Skin · corrodedDURING A HEAVY MX INSP EVENT, LWR WING PLATE HAS 2 AREAS OF CORROSION. CORROSION WAS REMOVED, AREAS WERE WITHIN LIMITS. RETURNED TO SERVICE.SDR ABXR200910020023Drain · crackedDURING A HEAVY MX INSP EVENT, MAIN ENTRY DOOR LWR DRAIN HAS 3 CRACKS GOING INTO IT. REMOVED, FABRICATED LWR DRAIN PLATE. RETURNED TO SERVICESDR ABXR200910020022Scuff Plate · crackedDURING A HEAVY MX INSP EVENT, MAIN CARGO DOOR CUT OUT AFT LWR STRUCTURE WAS DISCOVERED CRACKED AND GOUGED. REMOVED, FABRICATED AND REINSTALLED SCUFF PLATES. ITEM RETURNED TO SERVICE.SDR C8GA20090182Indicator · erraticDURING TAKEOFF ROLL THE CAPTAINS AIRSPEED INDICATOR BEGAN TO CYCLE FROM 0-300 KNOTS. THE TAKEOFF WAS ABORTED WHERE THE CREW RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND THE CAPTAINS AIRSPEED INDICATOR WAS REMOVED AND REPLACED. OPS CSDR ABXR200908250021Stop Fitting · crackedAFTER A POST C-CHECK TEST FLIGHT A CRACK WAS VISUALLY DISCOVERED ON THE L1 DOOR STOP IN UPPER AFT CORNER. THE CRACKED DOOR STOP FITTING WAS REMOVED, THE NEW STOP POSITION, DRILLED AND INSTALLED. THE STOP WAS ADJUSTED TO THE AMM. THE PRESSURIZATION LEAK CHECSDR ABXR200908240020Vent Line · misrepairedDURING A C-CK ROUTINE VISUAL INSP, INCORRECT LT WING VENT LINE CLAMPS WERE FOUND UNDER PANELS 7216 AND 7215. THE CLAMPS WERE EVALUATED BY ENGINEERING. REMOVED ORIGINAL CLAMPS AND INSTALLED BACC10CC20S CLAMPS. ITEM RETURNED TO SERVICESDR ABXR200908240019Vent Line · chafedDURING A C-CK ROUTINE VISUAL INSP, THE RT WING VENT LINE WAS FOUND CHAFED UNDER PANEL 7608. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040" AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TEST PERFORMESDR ABXR200908240018Support Angle · corrodedDURING THE ROUTINE VISUAL INSP OF THE UPPER SIDE OF THE RT NLG DOGHOUSE WAS FOUND CORRODED. THE CORROSION WAS CLEANED AND FOUND OUT OF LIMITS. THE UPPER SIDE ANGLE WAS REMOVED AND FABRICATED FROM 7075 T6511 EXTRUSION. THE ANGLE WAS CORROSION PROTECTED AND RESDR ABXR200908240017Fitting · damagedDURING THE REPETITIVE INSP NR 1 ENG PYLON SUPPORT FITTING IAW SB 2000-5410A0 2000-19-24, HOLES I, J, K, AND L WERE VISUALLY FOUND ELEGONGATED AND HOLES WERE FOUND PREVIOUSLY OVERSIZED TO MAX ALLOWABLE DIA. 0.2817 INCH. ENG MOUNT WAS REMOVED AND RE-INSTALLED ASDR ABXR200908240016Skin · damagedDURING A C-CK INSP, THE LT WING SKIN AT THE NR 1 SLAT OTBD TRACK CUT-OUT WAS HEAVYILY DAMAGED AND CRACKED DUE TO THE UPPER FWD SLAT ROLLER NOT BEING CAPTURED BY THE ROLLER BOLT. THE DAMAGED AREA WAS CUT-OUT AND A NEW SKIN SECTION WAS FABRICATED WITH 2024 T-3 SDR ABXR200908240015Skin · crackedDURING A C-CK REPETITIVE AD 2007-12-14 SB 727-53A0198, A CRACK WAS FOUND WITH EDDY CURRENT ON THE FWD ENTRY DOOR UPPER HINGE CUT-OUT. THE DAMAGE WAS CUTOUT TO A 0.70 INCH RADIUS, RE-INSPECTED WITH HFEC. FABRICATED SKIN FILLER FROM 2024 T-3 0.080 INCH, FABRICSDR ABXR200908240014Vent Line · dentedDURING A C-CK ROUTINE VISUAL INSP, THE RT WING VENT LINE WAS FOUND CHAFED ABOVE PANEL 7615. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040 INCH AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TEST PERFSDR ABXR200908240013Vent Line · dentedDURING A C-CK ROUTINE VISUAL INSP, THE LT WING VENT LINE WAS FOUND CHAFED ABOVE PANEL 7612. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040 INCH AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TEST PERFOSDR ABXR200908240012Line · dentedDURING A C-CK ROUTINE VISUAL INSP, THE LT WING FUEL DUMP LINE WAS FOUND DENTED ABOVE PANEL 7215. THE DAMAGE WAS CUT OUT, THE REWORKED AREA TREATED WITH ALODINE AND A DOUBLER FABRICATED FROM 5052-0 0.040 INCH AND COLD BONDED WITH BMS5-26 TYPE II. PRESSURE TESSDR ABXR200908240011Trunnion · corrodedDURING ROUTINE C-CK MX, THE LT TRUNNION FITTING WAS FOUND CORRODED OUTSIDE OF MM LIMITS INSIDE THE INNER BORE. THE LT AND RT TRUNNION FITTINGS WERE REMOVED AND REPLACED WITH NEW TRUNNIONS. NO OTHER DAMAGE OR CORROSION NOTED THE ITEM WAS RETURNED TO SERVICE.SDR ABXR200908240010Support Fitting · damagedDURING THE REPETITIVE NR 3 ENG SUPPORT FITTING INSP IAW SB 2000-5410A01, AD 2005-19-24, HOLES I, J, K AND L WERE VISUALLY FOUND ELONGATED AND THE HOLES WERE FOUND PREVIOUSLY OVERSIZED TO MAX ALLOWABLE DIA. 0.2817 INCH. FABRICATED FREEZE PLUGS FROM 15-5PH H1025SDR ABXR200908240009Gusset · crackedDURING THE ROUTINE VISUAL INSP OF A C-CK, THE MAIN CARGO DOOR JAMB LWR AFT GUSSET WAS FOUND GOUGED AND CRACKED IN SEVERAL PLACES. A REPLACEMENT GUSSET WAS FABRICATED FROM 2024 T3 0.063 INCH AND INSTALLED. THE ITEM WAS RETURNED TO SERVICE.SDR ABXR200908240008Structure · corrodedDURING THE ROUTINE VISUAL INSP OF A C-CK, THE SUBFLOOR WAS FOUND CORRODED OUT OF LIMITS. THE AREA WAS REPAIRED WITH A DOUBLER FABRICATED FROM 0.050 INCH, 2024 T-3. THE AREA WAS TREATED AND PRIMED FOR CORROSION PROTECTION. THE ITEM WAS RETURNED TO SERVICE.SDR ABXR200908210007Floorbeam · crackedDURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200908210006Floorbeam · crackedDURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200908210005Floorbeam · crackedDURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200908210004Floorbeam · crackedDURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200908210003Floorbeam · crackedDURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT INSP OF THE AEI CARGO DOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200908210002Floorbeam · crackedDURING THE ACCOMPLISHMENT OF A ROUTINE VISUAL AND EDDY CURRENT OF THE CARGO DOOR FLOOR STRUCTURE, THE FLOORBEAM SPLICE PLATE WAS FOUND CRACKED. THE SPLICE PLATE WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200908200001Support · corrodedDURING A HEAVY MX INSP EVENT, SUPPORT CLIP AT STR 26R CORRODED AT 545. REMOVED AND CLEANED SUPPORT CLIP AND FOUND OUT OF LIMITS. FABRICATED CLIP FROM 7075 T6 0.040 INCH. REINSTALLED CLIP. ITEM RETURNED TO SERVICE.SDR C8GA20090176B-Nut · brokenWHILE ACFT WAS PASSING THRU 26000 FT THE NR 3 ENG BEGAN TO COMPRESSOR STALL. CREW PERFORMED APPROPRIATE PROCEDURES AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE NR 3 ENG PRBC WAS REMOVED AND REPLACED. WHILESDR I5PA20090805Structure · corrodedDURING 5C CHECK AND INSP, CORROSION WAS FOUND BETWEEN BS 950C AND 950E AND STR 28L AND 28R. REPAIRED IAW EI-727-090705.SDR I5PA20090804Skin · damagedDURING 5C CHECK AND INSP, CORROSION WAS FOUND ON THE SKIN INTERNAL SURFACE WHICH WAS UNDER THE PREVIOUS SKIN REPAIR DOUBLER FROM BS 1009 TO BS 1045 AND BETWEEN S-27L AND S-28R. REPAIRED IAW EI-727-090704.SDR I5PA20090803Keelbeam · corrodedDURING 5C CHECK AND INSP, CORROSION WAS FOUND ON RT KEEL BEAM INBD FLANGE AFT OF BS740. AFTER BLENDOUT AND MEASURED ORIGINAL THICKNESS BLEND OUT EXCEED LIMITS. REPAIRED CORROSION IAW EI-727-090703 AREA WAS BLEND OUT AND TREATED WITH ALODINE AND DOUBLE PRIME ASDR I5PA20090801Spar · corrodedDURING 5C-CHECK AND INPS CORROSION WAS FOUND ON RT AND LT WING FRONT SPAR CHORD PLATE LWR SURFACE. AFTER BLEND OUT THE MAX LOSS OF MATERIAL THICKNESS WAS BEYOND THE ALLOWABLE LIMIT IAW SRM. FABRICATED AN INTERNAL REPAIR STRAP IAW EI-727-090701 HFEC ACCESSED SDR DHLA200900039Light · failedEMERGENCY EXIT LIGHT COCKPIT INOP. R & R EMERGENCY EXIT LIGHT ASSY. IAW MM 33-50-93 OPS CHECK OK.SDR CA090622005Window · cracked(CAN) JUST AFTER TAKEOFF, R1 WINDOW CRACKED EXTERIOR PANE WITH EVIDENCE OF BURNED HEAT ELEMENT. ACFT PROCEDED TO DESTINATION, NORMAL OPERATION, ACFT LANDED WITHOUT INCIDENT.SDR C8GA20090067Wire · brokenFLT 1740 FROM BNA TO CLT, DURING APPROACH THE NOSE LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED. THE RED LIGHT WAS ILLUMINATED AND THE GREEN LIGHT WAS OUT. THE CREW PERFORMED APPROPRIATE CHECK LIST AND LANDED WITHOUT INCIDENT IN CLT. POST FIGHT INSPECTIOSDR C8GA20090066Wire · chafedFLT 715 FROM MEM TO BNA, DURING SHORT APPROACH THE NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE RED LIGHT WAS ILLUMINATED AND THE GREEN LIGHT WAS OUT. THE CREW PERFORMED APPROPRIATE CHECK LIST AND LANDED WITHOUT INCIDENT IN BNA. POST FIGHT INSPECSDR C8GA20090065Accessory Unit · defectiveFLT 716 FROM BNA TO MEM, WHILE ON APPROACH INTO MEM THE NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. THE GREEN NOSE GEAR LIGHT WAS OUT, AND THE RED LIGHT WAS ILLUMINATED. AN ABORTED APPROACH WAS ACCOMPLISHED, CHECKLIST FOLLOWED AND AIRCRAFT LANDED IN MEM WISDR C8GA20090004Linkage · damagedFLT 1716 FROM TOL TO STL. DURING CLIMB OPERATION WHEN RETRACTING THE FLAP FROM 5 DEGREES TO 2 DEGREES THE NR 4 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. SDR C8GA20090003Position Switch · inoperativeFLT 2715 FROM IAH TO TOL. DURING CLIMB OPERATION WHEN RETRACTING THE FLAP FROM 5 DEGREES TO 2 DEGREES THE NR 4 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. SDR C8GA20080073Oil System · reads highFLT 706 FROM TOL TO MSP. DURING CRUISE OPERATION THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED. APPROPRIATE CHECKLIST WAS FOLLOWED AND THE ENGINE WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT IN MSP. POST FLIGHT INSPECTION WAS PERFORMED, FOUND NR 2 ENGISDR C8GA20080065Fire Loop · shortedFLT 716. ON DECENT THE APU FIRE LIGHT ILLUMINATED AND THE MASTER FIRE BELL SOUNDED. THE APPROPRIATE CHECKLIST ACCOMPLISHED. THE APU FIRE BOTTLE WAS DISCHARGED. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT TSDR CA081205006Stator · broken(CAN) DURING PUSHBACK ON C-FCJF EXCESSIVE FORCE WAS REQUIRED TO MOVE ACFT AND DETERMINED NR2 MAIN WHEEL WAS DEFLATED. ACFT PULLED BACK TO GATE FOR INVESTIGATION. MAINT WAS UNABLE TO REMOVE NR2 WHEEL. AFTER SEVERAL EFFORTS WITHOUT SUCCESS IT WAS DECIDED THE TISDR DHLA2008752001Skin · crackedNR 3 K-FLAP HAS TWO SEPARATE CRACKS AT BOTTOM CENTER JUST ABOVE BULLNOSE APPROX WS 171.5. REMOVED AND REPLACED NR 3 K-FLAP OPERATIONAL CHECK GOOD. IAW M/M 27-81-01.SDR C8GA20080103Stiffener · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE WING CENTER SECTION LOWER FORWARD STIFFENER ON FORWARD CHORD AT BS 740 LBL-45 CORRODED. CORROSION TO BE OUT OF LIMITS, REMOVED STIFFENER, FABRICATED NEW FROM 7075 T6 DIM 15 INCH AND INSTALSDR C8GA20080102Structure · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 3 SLAT OTBD STOP CUTOUT CORNER CRACKED. STOP DRILLED CRACK, PERFORMED HFEC WITH NO DEFECTS. FABRICATED DOUBLER FROM 2024 T3 .063 INCH DIM 9 INCH BY 9 INCH. INSTALLED REPAIR IAW SRM 57SDR C8GA20080101Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 686.50. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 686.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH SDR C8GA20080099Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 601.50. REPAIRED LT WING TANK FUEL VENT LINE AT WBL 601.50 IAW COTNEY ED NR EDAG52-1. FABRICATED DOUBLER FROM 2024 0.040 INCH DIM 1.625 INCH
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