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 FOTR2019813627Stringer · corroded(FOTR) BS 1130, STR 27 L HAS CORROSION AT STRINGER FITTING. CUT & REMOVED STRINGER 14 .7500" LONG FROM 1120 TO 1135 STR 27L. FABRICATED STRINGER REPAIR HAT SECTION MAT USED BAC 1498-145-7075-T6, PO 90010545 DIM 14.7500 LONG. SPLICE MAT. USED BAC 1498-131-7075-SDR FOTR2019813847Floorbeam · corrodedSTA 1130, FLOORBEAM LBL 0-9 FOUND CORRODED. CUT DAMAGE AREA AT LWR CHORD OF FLOORBEAM STA 1130 DIM. 5.75" X 2" IAW SRM 53-10-8, FIG 10. C/W HFEC INSP IAW NDTM PT6 51-00-00, FIG 23. DO DEFECTS NOTED. EXTENDED CUTOUT .040" NEW DIM 5.79 X 2" FAB 2EA ANGLES FROSDR FOTR2019813362Angle · damagedCRACK INBD AILERON, RT WING UPPER PANEL. REMOVED PANEL & CRACKED ANGLE AT INBD AILERON RT WING UPPER PNL IAW SRM 51-30-2. FABRICATED NEW ANGLE FROM 2024-T3. PO 900997 DIM. 5" X 2" IAW SRM 51-20-1, FIG 7 AND SRM 51-10-3 & SRM 51-30-6. TREATED AND PRIMMED IAWSDR FOTR2019813259Skin · damagedLT WING INBD FLAP, AFT FLAP HAS TEMP REPAIR C/W PERMINENT REPAIR IAW CUSTOMER REQUEST. REMOVED DAMAGED AREA; SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20 PAR 7. REPAIRED LT WING INBD AFT FLAP UPPER SURFACE BY HOT BONDING REPAIR ON IAW SERM 51-40-20, PARSDR FOTR2019813819Skin · damagedEVALUATE EXISTING DENT AT LT INBD FORE FLAP LOWER SURFACE, 28" FROM INBD EDGE. EVALUATED DENT ON LT INBD FOREFLAP LOWER SURFACE & DENT WAS FOUND TO HAVE SHARP CREASE & BEYOND ALLOWABLE LIMITS IAW SRM 57-50-1 FIG 3. REMOVED DAMAGE/ CLEANED & PREPARED AREA IAW SDR FOTR2019813648Skin · gougedDEEP GOUGE MARKS ON LT OTBD FORE FLAP AT INBD END L/E. BLENDED GOUGE OUT OF LIMITS IAW SRM 57-50-1 FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-4. MATERIAL USED 2024-T3 .063" PO 90010274 SIZE 3.5" X 4.25".SDR FOTR2019813595Web · damagedLT SIDE OF AIRSTAIR AREA, INSIDE FUSELAGE TORQUE BOX, WEB AT BS.1223 HAS DRILL DAMAGE IN UPPER INBD CORNER. CUT OUT DAMAGE AREA DIM. 1" X 1" IAW SRM 51-40-2. FABRICATED FILLER PO 9009504 AND DOUBLER FROM PO 9008186. TREATED AND PRIMED PARTS IAW SRM 51-10-2. ISDR FOTR2019813583Intercostal · damagedBS 950E-950F INTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 AFT CARGO. REMOVED INTERCOSTAL AT STA 950E-950F RBL4 IAW SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .040". PO 9009608. IAW SRM 53-10-2. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED INTERCOSTASDR FOTR/20198/13827Intercostal · damagedBS 970-990 INTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 IN AFT CARGO. REMOVED INTERCOSTAL AT STA 897-990, RBL 4 IAW SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .040". PO 9009608 IAW SRM 53-10-2. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED INTERCOSTSDR FOTR2019813826Intercostal · damagedINTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 IN AFT CARGO. REMOVED INTERCOSTAL AT STA 950F-970, RBL 4, IAW SRM 51-30-2. FABRICATED FROM 7075-T6 .040" PO 9009608 IAW SRM 53-10-2 TREATED AND PRIMED PART IAW SRM 51-10-2 INSTALLED INTERCOSTAL IAW SRM 51-30-2.SDR FOTR2019813466Intercostal · damagedBS 360 FRAME INTERCOSTAL HAS CORROSION AT FLOOR LEVEL LBL 60. REMOVED INTERCOSTAL FROM BS 360 FRAME IAW B727 SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .080 INCH. DIM 14.5 INCH BY 4 INCH, PO NR 9009647 IAW B727 SRM 523-10-2 FIG 7. TREATED AND PRIMED ISDR FOTR2019813271Frame Splice · chafedBS 1166 BETWEEN STRINGER 5 & 6 R GILLINER SUPPORT IS CHAFING AGAINST FRAME SPLICE. REMOVED FRAME SPLICE IAW SRM 51-30-2. FABRICATED FRAME SPLICE APPROX. DIM 8.3750" X 4.3750" IAW SRM 53-10-2, FIG 5 AND SRM 51-20-1, FIG 7. INSTALLED FRAME SPLICE AT BS 1166 BESDR FOTR20198913427Frame · damagedSTA 720E FRAME HAS FASTENERS W/ NO ED IN RT SIDE WINDOW AREA. CUTOUT DAMAGED AREA DIM. 1" X 3/4" IAW SRM 53-10-4, FIG 1. FAB. FRAME REPAIR 2EA PARTS MAT. USED 7075-0 .071" PO 90016396 DIM 13.5" X 3" & 13.5 X 4" IAW SRM 53-10-4, FIG 1 HEAT TREATED PARTS FROM 7SDR FOTR/20198/13440Frame · damagedSTA 720, FRAME HAS FASTENER W/NO ED IN WINDOW AREA ON LT SIDE. CUTOUT DAMAGE AREA DIM. 1" X .7500", FABRICATED FRAME REPAIR 2EA PARTS, MATERIAL USED 7075-0. PO 90016396, DIM 13" X 3" & 13" X 4" IAW. SRM 53-10-4. HEAT TREATED PART FROM 7075-0 TO 7075-T6. IAWSDR C8GA2010000072Floorbeam · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE FLOORBEAM FLANGE AT STA 1110 LBL 64. REMOVED CORROSION AND FABRICATED REPAIR ANGLES FROM 7075 T6, .090" DIM 13.5" X 4", 10.5" X 4" AND 4" X 1" FILLER INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SSDR C8GA2010000071Fitting · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE NLG RT TRUNNION FITTING HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000070Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE NOSE LANDING GEAR LT TRUNNION FITTINGS HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000069Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE LT MLG FWD TRUNNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2EA LOWER BUSHINGS AND 2EA UPPER BUSHINGS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000068Fitting · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE RT MLG FWD TRUNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2 EA LOWER BUSHINGS. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000067Shear Tie · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO STA 1148, BL 0 SHEAR-TIE IS CORRODED. REMOVED SHEAR-TIE AND FABRICATED NEW FROM 2024 T3 .050". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000066Floorbeam · corrodedDURING HEAVY MX IT WAS NOTED THAT THE MAIN CARGO FLOORBEAM IS CORRODED AT STA 1110 LBL 35. CORROSION WAS REMOVED, FABRICATED DOUBLER FROM 7075 T6 .090", FILLER FROM 7075 T6 .125. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000065Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STAT 1010, LBL 10 IS CORRODED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS FROM 7075 T6 .063" DIM 18" X 3", STRAP FROM 7075 T6 .100" DIM. 18" X 2" FILLER FROM BAC1505-100797 DIM. 7.25" X 2.25" AND INSTSDR C8GA2010000064Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STA 1030, RBL 20 IS CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000063Bulkhead · crackedDURING HEAVY MX, WHILE PERFORMING INSPECTIONS, IT WAS NOTED THAT THE RT INBD WHEEL WELL FWD BULKHEAD SKIN IS CRACKED AT APU OUTLET DUCT CUT-OUT LOWER. FABRICATED DOUBLER'S FROM 15-5PH .050". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVSDR C8GA2010000062Duct · corrodedDURING HEAVY MX, WHILE PERFORMING INSP, IT WAS NOTED THAT THE NR2 ENGINE "S" DUCT AT STATION 1203 6 O'CLOCK POSITION HAS CORROSION. REMOVED CORROSION AND FABRICATED REPAIR PARTS SPLICE STRAP FROM 301 1/2 HD , FABRICATED REPAIR DOUBLER FROM 7075 T6 .080". INSTASDR C8GA2010000061Skin · corrodedDURING HEAVY MX, WHILE PERFORMING INSPECTIONS, IT WAS NOTED THAT THE LT MLG WW INBD CTR CEILING AREA BL 0, STA 930 ABOVE APU SCREEN HAS CORROSION. REMOVED CORROSION AND FABRICATED DOUBLER FROM 2024 T3 .080" DIM 22" X 13". INSTALLED REPAIR, NO OTHER DEFECTS NOTSDR C8GA2010000060Web · dentedDURING HEAVY MX WHILE PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO DOOR FRAME AFT SIDE OF CUT-OUT AT BS 620 BETWEEN RBL 25-30 STRINGER 25R. REMOVED DAMAGE AND FABRICATED WEB REPAIR FROM 2024 T3 .040 DIM. 16.5" X 5". INSTALLED REPAIR, NO OTHER DEFECTSSDR C8GA2010000059Web · dentedDURING HEAVY MX PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO COMPARTMENT RT SIDE OF CARGO DOOR FRAME CUT-OUT AT BS 560 BETWEEN STR 23R & 25R. REMOVED DAMAGE AND FABRICATED WEB REPAIR FROM 7075 T6 .050 DIM. 15.5" X 5". INSTALLED REPAIR, NO OTHER DEFESDR C8GA2010000030Acm · inoperativeDURING CLIMB OPERATION, THE ACFT WAS UNABLE TO MAINTAIN CABIN PRESSURIZATION ON RT PACK. LT PACK WAS DMI. CLEANED CONNECTOR ON LT PACK TEMP BULB, R & R LT PACK FLOW CONTROL VALVE, RE RACKED AUTO PSI CONTROLLER, R & R LT ACM, R & R LT COMPRESSOR DISCHARGE OVESDR C8GA201000014Control Valve · inoperativeDURING CLIMB OPERATION WITH THE RT PACK ON DMI. THE LT PACK WOULD NOT MAINTAIN CABIN ALTITUDE. ACFT LEVELED OF AT 18,000 FT THE CABIN CONTINUED TO CLIMB AT A RATE OF 500 FT/MIN WITH CARGO HEAT OUTFLOW VALVE AND OUT FLOW VALVE CLOSED. THE ACFT RETURNED TO DEPARSDR ABXR20107130022Stiffener · corrodedDURING A SCHEDULED LINE MX EVENT, CORROSION WAS DISCOVERED WHILE ACCOMPLISHING OTHER MX ON A STIFFENER "C-CHANNEL" AT STA 312 OTBD AND AFT OF THE NLG TRUNNION LT SIDE. FABRICATED NEW STIFFENER FROM 7075-T76511 EXTRUSION AND REPLACED. ITEM WAS RETURNED TO SERVISDR C8GA201000011Controller · disconnectedDURING CLIMB OPERATION OUT OF SLW THE ACFT EXPERIENCED ERRATIC AND OFF-SCHEDULE PRESSURIZATION. ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, NOTING THE STATIC HOSE TO THE CABIN PRESSURE CONTROLLER WAS DISCONNECTED, CONNECTEDSDR C8GA201000010Cover · damagedAFTER STARTING THE TAKEOFF ROLE, THE UPPER YAW DAMPER "OFF" LIGHT ILLUMINATED. THE CREW PERFORMED AN ABORTED TAKEOFF AND RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT THE LIGHT COVER WAS STUCK IN SOCKET. PERFORMED GROUND TSDR ABXR201006050003Attach Angle · corrodedDURING THE ACCOMPLISHMENT OF A ROUTINE CPCP INSP CARD, A FAIRING ATTACH ANGLE WAS FOUND CORRODED BEYOND LIMITS. THE CORROSION DAMAGE WAS R & R WITH AN ANGLE FABRICATED FROM 0.050" 7075 T6 IAW THE SRM. THE ITEM WAS RETURNED TO SERVICE.SDR C8GA201000010AActuator · malfunctionedWHILE ON APPROACH WITH THE GEAR HANDLE IN THE DOWN POSITION THE NLG UNSAFE LIGHT ILLUMINATED. CREW PERFORMED APPROPRIATE CHECKLIST AND RECYCLED GEAR WITH ALL INDICATIONS NORMAL. ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R NLG LOCK ASDR ABXR201005260002Strap · crackedDURING A HEAVY MX EVENT THE LT WHEEL WELL STA 930 DECK STRAP WAS DISCOVERED CRACKED AND CORRODED JUST ABOVE THE HYD LINK CLUSTER. FABRICATED PRESSURE DECK STRAP FROM 2024-T3 .090 PO404503638 IAW SRM 53-1-02, FIG 5, SHEET 14, ITEM 164. ITEM WAS RETURNED TO SERVSDR C8GA201000004Duct · separatedFLT 2739 FROM ATL TO TOL. DURING CLIMB OPERATION AN AIRFRAME VIBRATION WAS NOTED AND ISOLATED TO THE NR 2 ENGINE. AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. IT WAS NOTED THAT THE 8TH STAGE DUCT SEPARATESDR C8GA20090298Actuator · malfunctionedDURING CLIMB OPERATION THE NR 7 L/E SLAT FAILED TO RETRACT. CREW PERFORMED REQUIRED CHECKLISTS AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, THE NR 7 SLAT ACTUATOR WAS DETERMINED TO BE AT FAULT. REMOVED AND REPLSDR C8GA20090297Beam · corrodedWHILE PERFORMING AN "A" MX CHECK, CORROSION WAS NOTED ON THE RT HORIZ STAB T/E UPPER BEAM APPROX 24" FROM HORIZ TIP. CORROSION WAS EVALUATED AND REMOVED, INSTALLED PERMANENT REPAIR 2024 T3 .063" DIM 3" X 12". NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TOSDR C8GA20090229Switch · dirtyDURING CLIMB OPERATION ON GEAR RETRACTION THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AND THE LT MLG DOOR LIGHT ON THE FE'S ANNUNCIATOR REMAINED ILLUMINATED. CREW CYCLED GEAR WITH NO HELP. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT.SDR ABXR200910060039Skin · delaminatedDURING A HEAVY MX INSP, THE LT WING NR6 SPOILER WAS FOUND DELAMINATED OUTSIDE OF THE MFG LIMITS. REMOVED AND REPLACED THE NR6 SPOILER AND ACCOMPLISHED THE ADJUSTMENT AND TEST IAW THE AMM. ITEM WAS RETURNED TO SERVICE.SDR ABXR200910060038Skin · delaminatedDURING A HEAVY MX INSP, THE LT WING NR2 SPOILER WAS FOUND DELAMINATED OUTSIDE OF THE MFG LIMITS. REMOVED AND REPLACED THE NR2 SPOILER AND ACCOMPLISHED THE ADJUSTMENT AND TEST IAW THE AMM. ITEM WAS RETURNED TO SERVICE.SDR ABXR200910060037Skin · crackedDURING A HEAVY MX INSP, IT WAS DISCOVERED THE FWD LOWER CARGO DOOR WAS DENTED AND CRACKED AT THE AFT LOWER CORNER. DOOR WAS REPAIRED. ITEM RETURNED TO SERVICE.SDR ABXR200910060036Web · nickedDURING A HEAVY MX INSP, MAIN CARGO DOOR CUT-OUT AFT WEB WAS DISCOVERED NICKED AND GOUGED. REPLACED LOWER WEB. ITEM RETURNED TO SERVICE.SDR ABXR200910060035Floor Support · corrodedDURING A HEAVY MX INSP EVENT CORROSION WAS FOUND ON A MAIN CABIN FLOOR SUPPORT. FLOOR SUPPORT WAS REPAIRED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200910060035ASupport · corrodedDURING A HEAVY MX INSP, IN COMPLIANCE WITH AD2001-20-09 AND DVI MAG PARTICLE S/B 57A0179 FOUND CORROSION ON THE LT AND RT LANDING GEAR FWD TRUNNION BEARING SUPPORTS. FWD TRUNNION BEARING SUPPORTS WERE REMOVED AND REPLACE. ITEM WAS RETURNED TO SERVICE.SDR ABXR20091005033Trunnion · corrodedDURING A HEAVY MX INSP, THE NOSE LANDING GEAR DRAG BRACE/ACTUATOR TRUNNION FITTING HAD CORROSION UNDER THE BEARING SURFACE. THE NOSE LANDING GEAR DRAG BRACE/ACTUATOR TRUNNION FITTING WAS REMOVED AND REPLACED. ITEM WAS RETURNED TO SERVICE.SDR ABXR200910050032Skin · crackedDURING A HEAVY MX INSP EVENT THE NR6 KRUGER LE FLAP WAS FOUND WITH 2 (EA) CRACKS MID AND OUT BOARD. THE FLAP WAS REMOVED AND REPLACED. ITEM RETURNED TO SERVICE.SDR ABXR200910030031Rib · crackedDURING A HEAVY MX INSP, THE LT WING OTBD FLAP INBD FAIRING AFT INTERANL RIB CRACKED IN 2 EACH PLACES. FABRICATED RIB FROM 2024 T3 0.063". HEATED TREATED RIB. INSTALLED RIB AND RETURNED ITEM TO SERVICE.SDR ABXR200910030030Rib · crackedDURING A HEAVY MX INSP, THE LT WING OTBD FLAP, OTBD FAIRING AFT INTERNAL RIB CRACKED. FABRICATED NEW RIB FROM 2024 O 0.065", AND HEAT TREATED. INSTALLED NEW RIB. ITEM RETURNED TO SERVICE.
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