Boeing 727-227
Service difficulty reports · 5,082
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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 = '727227' 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 = '727227' 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 08FDEA03889Skin · crackedDOOR L-1, INTERIOR AFT SKIN CRACKED AT 2 STOP PIN LOCATIONS (MKD). REPAIRED 2 DAMAGE AREA'S AT DOOR L-1 INTERIOR AFT SKIN STOP PIN LOCATIONS. HFEC IAW NDT MANUAL PART 6 51-00-00 FIG 23. TOOLING ID NR 0065 19 SEP 08. FOUND CRACKED. REMOVED DAMAGE AND REPAISDR 08FDEA03888Skin · damagedDURING STRINGER REPAIR AT FS 550 AND STR 26L EXISTING HOLE LOCATED IN STRINGER ONLY WAS DRILLED THRU FUSELAGE SKIN. THE HOLE THRU THE SKIN IS BETWEEN 2 MANUFACTURING SKIN FALLING ON THE EDGE OF THE FWD SKIN LEAVING NO EDGE DISTANCE. FABRICATED REPAIR DOUBLERSDR 08FDEA03852Support Beam · crackedLWR SIDE OF I/B SPOILER FITTING HAS MISSING AND LOOSE FASTENERS EVALUATED AND FOUND CRACK ON SPOILER SUPPORT BEAM. REPAIRED I/B SPOILER SUPPORT BEAM CRACK AT SPOILER FITTING AREA IAW FEDEX DRAWING NR: SR27-57-038 REV "C".SDR 08FDEA03821Beam · crackedRT WING T/E "J " BEAM IS CRACKED AT WBL 118 REMOVED T/E PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED "J" BEAM AS REQUIRED BY SRM 51-30-2. FABRICATED NEW "J" BEAM IAW DRAWIING NR 65-21655-10 REV "J". TREATED AND PRIMED AFFECTED PARTS IAW SRM 51-10- 2. INSTALLESDR 08FDEA03820Skin · damagedFUSELAGE LT, STATIC PORTS AREA HAS WORN AROUND EDGES AND POSITIVE STEP HEIGHT IS ON MAX LIMITS (0.006 INCH). REMOVED FASTENERS FROM AREA IAW SRM 51-30-2. FABRICATED DOUBLER AND TRIPLER IAW EA NR 7-5330-117032. TREATED AND PRIMED DOUBLER AND TRIPLER AND AFFESDR 08FDEA03793Skin · corrodedLOWER FUSELAGE STATION 1010 STRINGER 30 HAS AREA OF CORROSION ON EXTERIOR. REMOVED CORROSION AREA DAMAGED BEYOND LIMITS. NDT VERIFIED ORIG MATERIAL THICKNESS TO BE .071 "MATERIAL LOSS IS .009" REMAINING MATERIAL IS .062". FABRICATED REPAIR DOUBLER AND FILLERSDR 08FDEA03792Frame · damagedTOP OF FRAME DAMAGED UNDER "Z" FLOOR SUPPORT FS 540, RBL 7, WL 155. REMOVED DAMAGE AT TOP OF FRAME, NDT VERIFIED DAMAGE REMOVAL. FABRICATED REPAIR DOUBLER, TREATED AND PRIMED DOUBLER AND DAMAGED CUT OUT. INSTALLED REPAIR DOUBLER. REF SRM 51-40-3, FIG 1/SDR 08FDEA03791Frame · damagedTOP OF FRAME DAMAGED UNDER "Z" FLOOR SUPPORT, FS 520, RBL 7, WL 155. REMOVED DAMAGE AT TOP OF FRAME. NDT VERIFIED DAMAGE REMOVAL, FABRICATED REPAIR DOUBLER, TREATED AND PRIMED DOUBLER AND DAMAGE CUT OUT. INSTALLED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1, NDSDR 08FDEA03728Skin · damagedLT WING O/B FORE FLAP I/B SEQUENCE CARRIAGE HAS ELONGATED BOLT HOLES AT AFT END WBL 348 REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLESDR 08FDEA03727Skin · crackedNR 1 SLAT TRAILING EDGE IS GOUGED AND CRACKED AT I/B HOOK WS 716 TRIMMED OUT DAMAGED AREA DIM 1/2 PER 1/2 IAW SRM 57-50-3 FIG 10. FABRICATED REPAIR DOUBLER MAT USED 7075T6 0.125, DIM 4 INCH PER 3 1/2 INCH IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED IAW SRM 5SDR 08FDEA03726Skin · crackedCRACK TAIL SKID CUTOUT EXTERIOR SKIN STA 1214 TRIMMED OUT DAMAGED AREA DIM 1/4 PER 1/2 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR DOUBLER MAT USED 2024T3 0.050 IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG 1. TREATED AND PRIMED AREA AND REPAIR PART IAW SDR 08FDEA03725Floorbeam · damagedTOOL MARK AT FLOOR SUPPORT MAIN CABIN STA 328 TOP OF FRAME APROX 11" FROM I/B EDGE OF LWR SILL. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUTOUT DAMAGE AREA DIM 9 1/2 PER 2 INCH IAW B727 SRM 53-10-8 FIG 9. FABRICATED FILLER MAT USED 7075T6 0.071 AND 04 SDR CA080911006Engine · failed(CAN) AFTER T/O AND CLIMB OUT, NR2 ENGINE LOST OIL QTY AND OIL TEMP ROSE RAPIDLY INTO RED INDICATION. INFLIGHT SHUTDOWN COMPLIED WITH AND ACFT RETURNED TO DEPARTURE. NR2 ENGINE REPLACED IAW AMM AND KFL TASK CARDS, ACFT RETURNED TO SERVICE. ENGINE TO BE EVALUATSDR DHLA200800095Epr System · faultyWHEN SETTING T/O THRUST, NR 3 ENGINE PARAMETERS WERE SIGNIFICANTLY LOWER WITH EPR READINGS MATCHED. T/O REJECTED AT 80 KTS, TEMP 27, PA 3925 GW 160K. NR 3 ENG EPR SYSTEM DEFERRED REF B737 MEL 77-1-1. CAT A DDD 3.6.09. ALL ASSOCIATED ENG INDICATIONS NORMAL.SDR 08FDEA03651Stringer · corrodedFWD CARGO COMPARTMENT, STRINGER 27R CORRODED JUST FWD OF STA 720D APPROX 12 INCHES. REMOVED WEB IAW SRM 51-30-2. REMOVED DAMAGED AREA OF STRINGER IAW SRM 53-10-3. FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTSSDR 08FDEA03650Skin · corrodedFWD CARGO COMPARTMENT, SKIN UNDER STRINGER 28L IS CORRODED AT STA 662 JUST I/B OF EXISTING REPAIR CUTOUT. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 53-30-1 FIG 1. REMOVED EXISTING REPAIR IAW SRM 51-30-2. CUTOUT DAMAGED AREA DIM 5" PER 1 SDR 08FDEA03649Stringer · corrodedFWD CARGO COMPARTMENT, STRINGER 27R CORRODED JUST FWD OF STA 720D APPROX 12 INCHES. REMOVED WEB IAW SRM 51-30-2. CUTOUT DAMAGED AREA OF STRINGER IAW SRM 53-10-3. FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG1. TREATED AND PRIMED REPAIR PARTS ASDR 08FDEA03648Stringer · corrodedFWD CARGO COMPARTMENT, CORROSION ON STR AT BS 690, STR 27R. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND OUT OF LIMITS IAW SRM 53-10-1. CUTOUT DAMAGED AREA DIM 11" AND FABRICATED NEW STRINGER SECTION AND 02 EA SPLICES IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TSDR 08FDEA03647Skin · crackedCRACK ON DOUBLER AT RIGHT O/B FORE FLAP BY O/B TRUCK ATTACH FITTING AT WS 629. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PARTS, IAW SRM 57-50-4 FIG 7 AND 457-50-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-3SDR 08FDEA03631Skin · crackedCRACK AT FUSELAGE SKIN FWD OF STA 720D AND O/B OF STR 27R ABOVE RT RAM AIR DUCT REMOVED CTR FAIRING AT STA 720D, AIR DUCT AND 2 SUPPORT BRACKETS FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED AREA DIM 4" PER 3". FABRICATED REPAIR DOUBLER AND 2 REPAIR FILLERS ISDR 08FDEA03632Stringer · corrodedCORROSION INSIDE CHANNEL AND AT ATTACHING RIVETS STR 27L STA 1010 TO STA 1039 CUT OUT DAMAGED SECTION IAW SRM 53-10-31 FIG 1. FABRICATED 2 STRINGER SECTIONS AND 3 SPLICE SECTIONS IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED 2 STRINGESDR 08FDEA03616Spar · crackedRT WING O/B MID FLAP AFT SPAR, UPPER CHORD IS CRACKED AT WBL 332 REMOVED AND REPLACED RT O/B MIDFLAP ASSY IAW FX B727-200 MM 27-51-011-4. OPS CHECK GOOD IAW FX B727-200 MM 27-51-011-4 AND 27-51-000-5.SDR 08FDEA03609Skin · corrodedFWD CARGO COMPARTMENT, STR 26R IS CORRODED BETWEEN STA 720F AND STA 740 WITH EXFOLIATION REMOVED RT PACK CHECK VALVE AND DUCT IAW FEDEX MM 21-20-004 AND SRM 51-30-2. CUTOUT DAMAGED AREA DIM 10 1/2 INCH LONG. FABRICATED REPAIR FILLER FROM BAC1498-147 AND REPASDR 08FDEA03617Skin · chafedLT WING O/B FORE FLAP L/E REPAIR DOUBLER IS CHAFED (DAMAGED) AT WS 440 REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 57-50-2 FIG 4 AND SRM 57-50-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM SDR 08FDEA03614Seat Track · corrodedMAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK RBL 45 STA 380 STA 420 REMOVED 9G BULKHEAD AND ATTACHMENT PARTS FOR ACCESS IAW SRM 51-30-2 AND VENTURA SRM. REMOVED FLOOR PANELS IAW SRM 53-20-012. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SEAT TRACK AND ISDR 08FDEA03613Skin · corrodedFWD CARGO COMPARTMENT, FUSE SKIN IS CORRODED STR 28L FROM STA 660 TO STA 680 WITH EXFOLIATION CUTOUT DAMAGED AREA DIM 12.9 INCH AND FABRICATED REPAIR FILLER AND 2 REPAIR SPLICES IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AREA IAW SRM 51-10-2. SDR 08FDEA03612Skin · corrodedFUSELAGE SKIN HAS CORROSION BY CARGO HEAT OUTFLOW VALVE FLANGE AT STA 720D AND STR 30 REMOVED CENTER FAIRING AT STA 720D AIR DUCT AND 02 EA SUPPORT BRACKETS FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA DIM 4 INCH PER 3 INCH. FABRICATED REPAIR DOUBLER AND SDR 08FDEA03611Skin · damagedFUSELAGE LT SIDE SKIN BULGE AT STA 1030 AND STA 1010 AND STR 22L - STR 23L CUTOUT DAMAGED AREA DIM 8" PER 4 3/4" IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBLER AND AREA IAW SRM SDR 08FDEA03610Skin · dentedFUSELAGE LT SIDE DENT AT FWD OF STA 1130 STR 22L AND STR 21L CUTOUT DAMAGE AREA DIM CUTOUT 4 3/4 INCH PER 2 7/8 IAW SRM 53-30-3 FIG 3. FABRICATED DOUBLER REPAIR & FILLER IAW SRM 53-30-2 FIG 2, 53-30-3 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED RESDR C8G2008F00016Line · leakingON ROTATION THE NR 3 ENGINE FAILED. THE CREW PERFORMED APPROPRIATE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AC RETURNED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, IT WAS NOTED THAT THE FUEL FEED LINE TO THE P & D VALVE WAS LEAKING. TSDR PCS2008F00000Compressor · failedDURING CLIMB BETWEEN 180 TO 210 FLIGHT LEVEL NR 1 ENG COMPRESSOR STALL FOLLOWED BY OIL TEMP RISE. AFTER SECOND COMPRESSOR STALL NR 1 ENG OIL PRESS LIGHT ILLUMINATED. ENG WAS SHUT DOWN PER AOM. NR 1 ENG OPERATED APPROX 9 MINUTES OIL PRESS ABOUT 20 PSI. POSTSDR C8G2008F00009Connector · dirtyAFTER TAKEOFF, DURING CLIMB, OPERATION, THE NR 8 SLAT WOULD NOT RETRACT. POST FLIGHT INSP WAS PERFORMED AND THE NR 8 SLAT ACTUATOR CONNECTOR WAS CLEANED AND SYSTEM WAS OPERATIONAL CHECKED WITH NO DEFECTS. NO OTHER DEFECTS WERE NOTED. AC WAS RETURNED TO SERVISDR DHLA200800082Compressor · stalledENG FAIL LIGHT/AUTO PACK TRIP LIGHT FAILED AS THRUST APPLIED FOR T/O. RAN APPROPRIATE PROCEDURE IN AOM. CONTACTED MX AND DISPATCH. ALL INDICATIONS NORMAL AFTER PROCEDURE, APPARENT COMPRESSOR STALL AS THRUST APPLIED. NOTE, CREW REPORTED HEAVY CROSSWINDS DURSDR FDEA200807112821Line · crackedAT FL 320 "A" SYS QUANTITY DECREASED TO ZERO. RAN QRH FOR HYD SYS "A" LEAK CHECKS PERFORMED. MANUAL GEAR EXT AND ALT FLAPS LANDING. SYS "A" FLUID SHUTOFF WAS CLOSED AT 05:09, ENGINE SHUTDOWN AT 05:51. FOUND THE NR 2 SPOILER RETURN LINE CRACKED. WORKING OSDR 08FDEA02821Line · crackedAT FL 320 "A" SYS QUANITY DECREASED TO ZERO. RAN QRH FOR HYD SYS "A" LEAK CHECKS PERFORMED. MANUAL GEAR EXT AND ALT FLAPS LANDING. SYS "A" FLUID SHUTOFF WAS CLOSED AT 05:09, ENGINE SHUT DOWN AT 05:51. FOUND THE NR 2 SPOILER RETURN LINE CRACKED. WORKING OSDR DHL2008F00003Module · smokeWHILE SWITCHING AC VOLT SELECTOR SWITCH FROM EXTERNAL TO APU, SMOKE CAME FROM BEHIND BACK OF PNL AND VOLT AND FREQ GAGES BECAME INOP IN ALL POSITIONS, NO RESIDUAL EITHER. REMOVED AND REPLACED AC METER MODULE ASSY IAW 24-20-00. OPS CHECKS NORMAL IAW SAME DURISDR 08FDEA02792Skin · dentedNR 1 SLAT UPPER SURFACE HAS ONE DENT AT WS 760.SDR 08FDEA02789Frame · damagedSCREW MARKS ON FRAME 1110 AT STR 27R AND 27L UNDER TIE DOWN POINTS.SDR 08FDEA02750Roller · out of adjustON DESCENT TO IAD AIRFRAME BUFFET AT 290 KNOTS 270FL FOLLOWED QRH AT 14,000 250 KTS NO BUFFET FELT. FLAPS 15 DEGREES LANDING ACCOMP FOR WING LEVEL NEED 1/2 UNIT OF TRIM RUDDER. CONTROL WHEEL SHOWED 35 DEGREES RIGHT WITH NO TRIM. OPS CHECK SPOILERS ALL DEPLSDR 08FDEA02724Keelbeam · crackedRT WHEEL WELL INBD SIDE ON 870 BULKHEAD AND KEEL BEAM CHORD CRACKED. REMOVED AND REPLACED RT WHEEL WELL BS 870 BULKHEAD CHORD WITH NEW CHORD PO NR 819337 IAW B727 SRM 51-30-5 AND SRM 51-30-2.SDR 08FDEA02715Skin · crackedRT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED RT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKED. STOP DRILLED CRACK DIMS .250 IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL IAW NDTM PT 6 51-00-00 FIG 23 CRACK TERMINATES IN STOP DRILL HOSDR 08FDEA02714Skin · crackedLT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED LT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKED. STOP DRILLED CRACK IAW SRM 51-10-1 DIMS .250. HFEC INSPECTED STOP DRILL IAW NDTM 51-00-00-FIG 23 CRACK TERMINATES IN STOP DRILL HOLE. SDR 08FDEA02467Angle · crackedRT WING L/E STA 90 VERTICAL ANGLE CRACKED LWR SIDE. FABRICATED REPAIR ANGLE FILLER FROM 7075-T6 .050 PO NR 9007294 DIMS 7 INCH BY 2 1/2 INCH, FILLER 2 INCH BY 1 INCH. INSTALLED REPAIR PARTS AT RT WING LE STA 90 IAW SRM 51-40-3 FIG 1, SRM 57-20-2 FIG 1 AND SRSDR 08FDEA02466Skin · dentedLT FWD FUSELAGE STA 190 STR 27L REPAIR DOUBLER HAS SKIN BULGES AND DENTS. CUTOUT DAMAGED AREA DIMS 1 1/4 INCH BY 1 1/2 INCH IAW SRM 53-10-3 FIG 5. FABRICATED DOUBLER REPAIR USING 2024-T3 .050 PO NR 9006288 DIMS 10 1/2 INCH BY 13 1/2 INCH AND FILLER USING 202SDR 08FDEA02460Stringer · corrodedSKIN BULGE JUST FWD OF STATION 1010 STR 27L. REMOVED FASTENERS FROM AFFECTED AREA IAW SRM 51-30-2, CUTOUT STRINGER SECTION (DIM 10 1/4" LONG) IAW B727 SRM 53-10-3 FIG 1, REMOVED EXISTING SPLICE IAW SRM 51-30-2, FABRICATED REPAIR PARTS IAW SRM 51-10-2, CLEANEDSDR 08FDEA02461Skin · dentedDENT IN LEFT FWD FUSELAGE STA 545 ABOVE STR 24L (RVSM AREA). REPAIRED DENT IAW EA 7-5330-116991.SDR 08FDEA02452Bolt · damagedNR 3 ENGINE STARTER CONTROL ROD INBD OF ENGINE, NUT HAS NO THREADS SHOWING AND SPRING CLIP NOT BENT OVER BOLT HEAD. PROPERLY INSTALLED NR 3 ENG START CONTROL ROD (UPPER) BOLT AND ATTACHING HARDWARE IAW FX MM 76-11-021-2.SDR 08FDEA02459Bulkhead · crackedCRACK IN RIGHT WHEEL WELL 870 BULKHEAD BOTTOM SIDE OF APU BLEED VALVE DUCT CUTOUT. FABRICATED REPAIR DOUBLER IAW SRM 53-10-9, & FILLER, INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIG 5.SDR 08FDEA02458Control Cable · twistedOUTBOARD FLAP TRANSMITTER CABLE TWISTED AROUND (2 EACH) LT WING SPOILER CABLES. RE-ROUTED LT O/B FLAP TRANSMITTER CABLE WHICH WAS WRAPPED AROUND 2 EACH SPOILER CABLES IAW MM 27-52-013-4. NO DEFECTS NOTED TO SPOILER OR FLAP TRANSMITTER CABLE. OPS CHECK GOOD ISDR 08FDEA02422Door Frame · corrodedAFT PIT DOOR OPENING AFT FRAME STA 990 IS CORRODED ON LOWER SURFACE OF FRAME, UPPER ANGLE BETWEEN STR 26R AND STR 27R REMOVED CORROSION, FORMED REPAIR ANGLE, HEAT TREATED AND CAD PLATED REPAIR ANGLE. INSTALLED REPAIR ANGLE. REFERENCE EA NR 75310-113992.
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