Boeing 727-2S7
Service difficulty reports · 555
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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 = '7272S7' 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 = '7272S7' 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 C1HA200685003Floorbeam · corrodedCORROSION ON CABIN FLOORBEAM 380 RBL 15 TO 48. FOUND CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1. CUT OUT DAMAGE AREA IAW B727 SRM 51-10-1. FAB UP CHORD FROM 7075 T6, ANGLE STRAP IAW B727 SRM 53-10-8 FIG 3. ALODINE & PRIME IAW B727 SRM 51-10-2. INSTALLEDSDR C1HA200683001Floorbeam · corrodedCABIN CORROSION FLOORBEAM 344 LBL 48 TO RBL 12. FOUND CORROSION OUT OF LIMIT IAW B727 SRM 53-10-1. REMOVED DAMAGED AREA, FABBED UPPER CHORD FROM BAC 1505-29221 ANGLE FROM BAC 149-2831 IAW B727 SRM 53-10-2 FIG 7. ALODINE & PRIME IAW B727 SRM 51-10-2, INSTALLSDR C1HA200685004Seat Track · corrodedCORROSSION CABIN SEAT TRACK LBL 24 STA 380 TO 440. REMOVED DAMAGE TRACK IAW B727 SRM 51-30-2, FABBED NEW TRACK FROM BAC 1520-792-7178 T6 IAW B727 SRM 53-10-2 FIG 7. ALODINE & PRIME IAW B727 SRM 51-10-2, INSTALLED SEAT TRACK IAW B727 SRM 53-10-5 FIG 7.SDR C1HA200681003Bracket · chafedAFTER T/O STL, UPON GEAR RETRACTION LEFT MAIN GEAR DOOR LIGHT STAYED ILLUMINATED. LEFT MAIN GEAR LIGHT WOULD GO OUT INITIALLY THEN COME BACK ON. CLIMBED TO 8000 FT, DUMPED APPROX 17,900 LBS FUEL. RAN CHECK LIST IN ACCORDANCE WITH COM AND RETURNED TO STL, NOSDR 1HA200681002Line · crackedDURING FLIGHT THE NR2 (B) SYSTEM HYDRAULIC LOW PRESSURE LT ILLUMINATED FOLLOWED BY THE B SYSTEM NR 1 LOW PRESSURE LT ILLUMINATING AND LOSS OF B SYSTEM HYDRAULIC PRESSURE , THE B SYSTEM QUANTITY GUAGE INDICATED FULL THE ENTIRE FLIGHT. HYDAULIC BRAKE PRESSURE SDR C1HA200682006Seat Track · corrodedBS 1010-1070 LBL 45 CABIN SEAT TRACK CHANNEL HAS CORROSION & IS CRACKED ON O/B FLANGE BS 1070. REMOVED SEAT TRACK LBL 45 BS 1010-1070 IAW B727 SRM 51-30-2, FABRICATED SEAT TRACK USING BAC1520-792 7178-T6, DIM 79 INCHES IAW B727 SRM 53-10-1 FIG 7. ALODINE ANDSDR C1HA200682001Seat Track · corrodedBS 1010-1030 RBL 45 CABIN SEAT TRACK TOP & O/B FLANGE HAVE CORROSION. FOUND CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED DAMAGED TRACK FROM STA 950F TO 1030 RBL 45 IAW 727 SRM 51-30-7, FABRICATED NEW TRACK FROM BAC1570-792 7178 T6, DIM 80 INCHSDR C1HA200682002Beam · crackedSTA 1183 BULKHEAD, VERTICAL BEAM AT RBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-15, PER S/B 727-53-0192 FIG 2 REV 1 DATED MAY 30/91.SDR C1HA200682009Floorbeam · corrodedFLOORBEAM BS 344 HAS CORROSION. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA, FABBED FILLER, 7075-T6, .080, 1 X .1875 INCH (2EA) REPAIR ANGLES 7075-T6, .071, 16.5 X 1.875 INCH, & 2 EA SAME MAT 14.5 X 1.875 INCH IAW B727 SRM 53-10-2 FIG 7SDR C1HA200682007Floorbeam · corrodedBS 1030 RBL 4 - 10 LBL CABIN FLOOR SUPPORT UPPER FLANGE HAS CORROSION. CUT OUT DAMAGE AREA AT BS 1030 RBL 20 TO LBL 10 IAW B727 SRM 51-10-1, FABRICATED T-SUPPORT USING BAC1505-100617, DIM 43.125 X 2.25 INCH, 2 EA SUPPORT ANGLE AND TWO STRAP IAW B727 SRM 53-10SDR C1HA200682010Skin · bulgedFUSELAGE EXTERIOR BS 1075 STRINGER 29 RT AT FWD END OF REPAIR DOUBLER HAS SKIN BULGED WITH POPPED RIVET. CUT OUT DAMAGED SKIN, FABBED AND INSTALLED FILLER (2024-T3 .063, DIM 1.5 X 1 INCH) AND DOUBLER (2024-T3 .080, DIM 43.25 X 14.625 X .625 INCH) IAW 727 SRM SDR C1HA200682013Stringer · corrodedAFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1030 THRU BS 1050 CORROSION SPOTS BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED STRINGER, MATERIAL USED BAC1498-145, DIM 17 INCHES IN LENGTH IAW 727 SRM 53-10-3 FIG 1. NO CORROSION NOTEDSDR C1HA200682014Web · crackedRIGHT WHEEL WELL BS 870, WEB IS CRACKED FROM APU LOAD CONTROL VALVE ACCESS CUTOUT. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS, FABBED FROM 15-5 PH STEEL, DIM 21 X 18.5 INCHES AND 10.75 X 11.25 INCHES IAW 727 SRM 53-10-9 FIG 5.SDR C1HA200682016Floor Support · bulgedCOCKPIT FLOOR SUPPORT AT FS 303 & LBL 12 IS BULGED. REMOVED, FABBED NEW & INSTALLED FLOOR SUPPORT IAW B727 SRM 53-10-2 FIG 7 & 51-30-2.SDR C1HA200682012Stringer · corrodedAFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1010 THRU BS 1030 SPOT OF CORROSION BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED DAMAGED STRINGER, MATERIAL USED BAC1498-145, DIM 18 INCHES IN LENGTH IAW 727 SRM 53-10-3 FIG 1. NO CORROSDR C1HA200682005Seat Track · corrodedBS 1030-1090 LBL 24 CABIN SEAT TRACK O/B UPPER FLANGE IS CORRODED. REMOVED AND REPLACED SEAT TRACK LBL 24 BS 950-1090 WITH BAC 1520-792, DIM 129.5 INCH IAW 727 SRM 53-10-5 FIG 1.SDR C1HA200682004Vertical Beam · crackedSTA 1183 BULKHEAD, VERTICAL BEAM AT LBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-14, PER S/B 727-53-0192 FIG 2 REV 1 DATED MAY 30/91.SDR C1HA200682003Seat Track · corrodedBS 1030-1120 RBL 24 CABIN SEAT TRACK HAS SMALL AREAS OF CORROSION. REMOVED DAMAGE TRACK BS 1010 - 1130 RBL 24 IAW B727 SRM 51-30-2. FABRICATED NEW TRACK P/N BAC1520-7927178-T6, DIM 126 INCH FROM STA 1010 TO 1130 IAW B727 SRM 53-10-1 FIG 7. ALODINED AND PRIMSDR C1HA200682015Stiffener · crackedRIGHT WHEEL WELL BS 870 & KEEL BEAM VERTICAL STIFFENER CRACKED (NDT CONFIRMED). REMOVED AND REPLACED DAMAGED STIFFENER P/N 65-18636-378, IAW 727 SRM 51-30-2.SDR C1HA200682008Floorbeam · corrodedBS 1110 LBL 24 - RBL 24 TRANSVERSE FLOOR SUPPORT UPPER FLANGE HAS CORROSION (BOTH SIDES). REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. REMOVED LBL 24 TRACK IAW B727 SRM 51-30-2, FABRICATED T-ANGLE 60 INCH DIM 4 ES STRAP DIM 15", 11", 14" AND 10.5". FOUR EASDR C1HA200682011Stringer · corrodedAFT PIT STRINGER 29R CORRODED AT BS 1075. REMOVED AND REPLACED DAMAGED STRINGER SECTION MATERIAL USED BAC1498-147, DIM 18.375 INCH LENGTH IAW 727 SRM 53-10-2 FIG 9 & 53-10-3 FIG 1.SDR C1HA200681001Unknown · unknownPERFORMED W/S ESCAPE MANUEVER AT MAF (ARRIVAL) WITH FIREWALL POWER ON ALL 3 ENGINES. NO ENGINE LIMITATIONS WERE EXCEEDED. PERFORMED INSPECTION OFF ALL ENGINES INLET AND EXHAUST PER B727 MM 72-00-00. NO DAMAGE FOUND. A/C OK FOR SERVICE.SDR C1HA200686001Support Fitting · crackedNR 3 ENGINE PYLON; DURING OPEN HOLE HFEC OF FWD SUPPORT FITTING PER TASK CARD AD 2005-19-24-02, FOUND CRACK IN HOLE P OF ANGLE 69-16977-2. REMOVED AND REPLACED FWD SUPPORT FITTING PART 69-16977-2 REF BAC PRINT 65 -72772.SDR C1HA200581019Attach Angle · crackedWHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON FIREWALL ATTACH ANGLE P/N 69-16977-1 CRACKED NEXT TO MOUNT FITTING. REMOVED AND INSTALLED ATTACH ANGLE P/N 69-16977-1 REF BOEING PRINT 65-72772.SDR C1HA200581018Controller · malfunctionedCLIMBING THROUGH FL290, NOTICED CABIN ALTITUDE RAPIDLY CLIMBING, ALTITUDE HORN THEN CAME ON, COULDN'T CONTROL CABIN, PERFORMED COM PROCEDURE 2.21.5 & THEN PERFORMED COM PROCEDURE 2.21.3. MAINTENANCE IS CURRENTLY TROUBLESHOOTING SYSTEM.SDR C1HA200568004Frame · corrodedUPPER FRAME CHORD CORRODED ON LWR SURFACE IN AFT PIT BS 990 OVER STR 27R JUST BEHIND AFT DOOR CUTOUT. CUT OUT DAMAGED AREA FABBED AND INSTALLED FILLER 2" BY 1" AND DOUBLER ANGLE 8 3/4" BY 3 1/4" FROM 10134-3001 7075 T6 PO NR 9001253 IAW 727 SRM 51-40-4 FIG 1.SDR C1HA200568003Channel · crackedNLG LOCK ACTUATOR SUPPORT CHANNEL IS CRACKED BY LWR INB SUCTION VISUAL AND HFEC CONFIRMED. REMOVED AND REPLACED NLG LOCK ACTUATOR SUPPORT CHANNEL PN 69-19122-2 PO NR 535313 IAW 727 SRM 51-30-2. REMOVED DAMAGED FITTING CHANNEL IAW 727 SRM 51-30-2.SDR C1HA200586001Support Bracket · corrodedRT NLG LOCK ACTUATOR SUPPORT BRACKET HAS NUMEROUS GOUGES CORROSION IN ONE OF THE BOLT HOLES AND WORN BUSHING. REMOVED AND REPLACED RT AND LT NLG LOCK ACTUATOR SUPPORT BRACKETS IAW B727 MM 32-33-11.SDR C1HA200586002Frame · corrodedFRAME LEG CORRODED IN FWD PIT AT FRAME 700 BETWEEN STRINGERS 28L AND 29L. CUT OUT DAMAGED AREA FABBED AND INST REPAIR DOUBLER AND ANGLE MADE FROM 7075 T6 .050 PO NR 9002126 DIM DOUBLER 6" BY 4 1/2" AND ANGLE 7" BY 2" IAW B727 SRM 53-10-4 FIG 11. OPENED WTB PSDR C1HA200568005Stiffener · crackedRT WHEEL WELL BS 870 AND KEEL BEAM VERTICAL STIFFENER CRACKED NOT CONFIRMED. REMOVED AND REPLACED DAMAGED ANGLE PN 65-18636-378 PO NR 535322 IAW 727 SRM 51-30-2, LEAK CHECK PERFORMED ON POST CHECK RUN SHEET M-054.SDR C1HA200581012Stiffener · crackedU-CHANNEL SUPPORT IS CRACKED ON AFT SIDE OF WEB INSIDE OF RT LOWER TORQUE BOX, STA 1263 + 10 IN. REMOVED AND REPLACED DAMAGED BEAM P/N 65-17518-8, PO 531836 AT RT LWR TORQUE BOX AT ACTUATOR SUPPORT FITTING IAW SB 727-53-0129 REV 5 FIG 4 RII ACCOMPLISHED.SDR C1HA200581015Frame · dentedFRAME DENTED IN FWD CARGO PIT STA 680 OVER STRINGER 25R, MARKED. CUT OUT DAMAGED AREA DIM 1.375 X .875 INCHES AND FABBED ANGLE REPAIR FROM 7075T6 .063 PO9002507 DIM 15.75 X 3.75 IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ANGLE TREATED AND PRIMED INSTALLED SDR C1HA200581017Stiffener · crackedRIGHT MLG KEELBEAM INBOARD SIDE VERTICAL STIFFENER IS CRACKED STA 870 (MARKED). REMOVED AND REPLACED DAMAGED VERTICAL STIFFENER BS 870 AT KEEL BEAM IAW 727 SRM 51-30-2 P/N 65-18036-378 PO 53185.SDR C1HA200581016Frame · dentedFRAME DENTED IN FWD CARGO -B- STA 660 OVER STRINGER 26R, MARKED. CUT OUT DAMAGED AREA DIM 2.125 X 1 INCH, FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002126 DIM 13 X 4 INCHES IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED AND PRIMED INSTALLEDSDR C1HA200581014Skin · crackedAFT CARGO DOOR HAS CRACK ABOVE THE FWD BLOW OUT PNL BS 950E INNER SKIN. CUT OUT DAMAGED AREA DIM 2 X .5 INCH AND FABBED DOUBLER FROM 7075T6 .050 PO 9002507 DIM 3.5 X 3 INCHES IAW 727 SRM 52-30-1 FIG 5 AND 51-40-2 FIG 1. DOUBLER TREATED, PRIMED AND INSTALLED SDR C1HA200581013Angle · crackedL-ANGLE SUPPORT IS CRACKED AT UPPER INBOARD CORNER OF RIGHT LOWER TORQUE BOX, STA 1263 + 10 INCHES. REMOVED AND REPLACED DAMAGED ANGLE P/N 65C13874-4 PO 3146138 AND FILLER P/N 65C13874-5 PO 3146132 AT RIGHT LOWER TORQUE BOX AT ACTUATOR SUPPORT FITTING IAW SB SDR C1HA200581002Frame · crackedCRACK ON FRAME AT BS 804 STR 15R. CUT OUT DAMAGED SECTION, FABBED NEW FILLER AND SPLICE ANGLE FROM 7075T6 .090 PO 294560 DIM FILLER 6.5" X 1" X 1" AND SPLICE 11.75 X 1 X 1, TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1 RII ACCOMPLISHED.SDR CIHA200581006Frame · dentedFWD CARGO PIT HAS FRAME DENTED AT STA 520 STR 25R (MARKED). DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA BS 520. FRAME BETWEEN STR 25R-26R DIM 2 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002351 DIM 9.25 X 4 INCHES, SDR C1HA200581011Channel · crackedU-CHANNEL SUPPORT IS CRACKED ON FWD SIDE OF WEB INSIDE OF RIGHT LOWER TORQUE BOX, STA 1263 + 10 INCHES. REMOVED AND REPLACED DAMAGED GUSSET P/N 69-67881-1 PO 5070544 AND STIFFENER P/N 65-17518-15 PO 531824 AT RIGHT LOWER TORQUE BOX AT ACTUATOR SUPPORT FITTINGSDR C1HA200581010Web · crackedRIGHT LOWER TORQUE BOX HAS CRACK AT LIGHTNING HOLE WITH STOP DRILL HOLE, STA 1243 +6 IN. ROUTED OUT DAMAGED AREAS, FABBED DOUBLER FROM 7075 T6 .032 PO 900573 DIM 10 X 2 INCHES IAW 727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. DOUBLER TREATED AND PRIMED AND INSTALSDR C1HA200581009Frame · crackedRIGHT MLG WW LOAD APU CONTROL VALVE CUT OUT HOLE ON STA 870, WEB IS CRACKED. CRACK STOP DRILLED IAW 727 SRM 51-10-1. FABBED AND INSTALLED 2 EA DOUBLERS FROM 301 1/2 HD .050 PO 9912793 DIM 12 X 11 INCHES AND 18.5 X 21 INCHES IAW 727 SRM 53-10-9 FIG 5.SDR C1HA200581007Skin · dentedBS 463 BETWEEN 15RT-16RT STRINGERS HAS LARGE PROTRUDING DENT OIL CANNING. DAMAGE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA, FABBED FILLER FROM 2024 T3 .040 PO 9002416 DIM 4.375 X 4.5 INCH, DOUBLER FROM 2024 T3 .050 PO 9002507 DIM 14.25 X 1SDR CIHA200581005Frame · dentedFWD CARGO PIT, HAS FRAME 520 DENTED ON STR 26R. DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA BS 520 FRAME BETWEEN STR 25R AND 26R DIM 2 X 1 INCH, FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002351 DIM 9.25 X 4 INCH, TREATED, PRIMEDSDR C1HA200581004Frame · dentedFRAME DENTED IN FWD CARGO PIT OVER BS 680 OVER STRINGER 25R, MARKED. CUT OUT DAMAGED AREA 1.75 X .75 INCH AND FABBED REPAIR DOUBLER FROM 7075T6 .063 PO 9002351 DIM 9.75 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED AND PRIMED SDR CIHA200581003Clip · crackedSUPPORT CLIP ON STR 16R CRACKED AT BS 850. REMOVED DAMAGED SPLICE ON STR 16R AT BS 850 IAW 727 SRM 51-30-2. FABBED NEW SPLICE FROM BAC 1498-137 PO 4496178 DIM 6 INCHES IN LENGTH IAW 727 SRM 53-10-2 FIG 9. SPLICE TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51SDR C1HA200581008Frame · dentedFRAME DENTED IN FWD CARGO PIT STA 700 OVER STRINGER 25R, MARKED. CUT OUT DAMAGED AREA DIM 3 X .625 INCH AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002351 DIM 11 X 3. .875 INCH IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ANGLE TREATED, PRIMED AND INSTALLEDSDR C1HA200581001Regulator · malfunctionedAFTER DEPARTURE, RIGHT PACK TRIPPED FOLLOWED BY NR 3 BLEED TRIP. TRIPPED AGAIN COM 21.15 AND 2.36.2 AFTER COM PROCEDURE. REMOVED AND REPLACED RT HIGH PRESSURE REGULATOR PER M/M 36-12-51, OPS CHECK NORMAL PER M/M 36-12-01.SDR C1HA200583002Compressor · stalledNR 2 ENGINE COMPRESSOR STALL DURING APPROACH WHILE FULLY CONFIGURED AND 1.4 EPR PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST. PERFORMED ENGINE RUN AT VARIOUS POWER SETTINGS. PERFORMED ACCEL AND DECEL CHECK. CHECKED ANTI-SURGE BLEED VALVE SCHEDULING ALL PARSDR C1HA200582001Window · crackedENROUTE WINDOW CRACKED, REPLACED R2 WINDOW REF 56-12-11 AND AJUSTED AND OPS CK GOOD.SDR C1HA200585001O-Ring · failedEXPERIENCED RAPID DECOMPRESSION AT FLT 310, RAN COM RAPID DECOMPRESSION AND DESCENT CHECK LIST. CABIN STABILIZED AT 17,000 FT, FOUND LT FWD CLAMP LOOSE ON WATER SEPARATOR. REMOVED AND INSPECTED CLAMP, FOUND SERVICEABLE. INSTALLED NEW O-RINGS, REINSTALLED LT
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