Boeing 727-30C
Service difficulty reports · 931
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 = '72730C' 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 = '72730C' 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 DHL9770390DSeat Track · wornD-CHECK, AFT SEAT TRACK WORN AT F/E STATION. REMOVED AND REPLACED F/E SEAT TRACK PER SRM 51-30-2.SDR DHL9770389DFrame · crackedD-CHECK, STA 480, ABOVE STR17R, INBOARD FLANGE OF RIB IS DENTED. CUTOUT DAMAGED AREA 3 BY 1 AT FRAME REPAIR BS 480, STR17R PER SRM 53-10-4. INSTALLED FRAME REPAIR AT STA 480, STR17R, PER SRM 53-10-4. REPAIR SIZE 11 BY 6.SDR DHL9770388DFrame · crackedD-CHECK, STA 500, ABOVE STR17R, INBOARD FLANGE OF RIB DENTED. CUT OUT DAMAGED SECTION 1.25 BY 4 OF RIB AT BS500, ABOVE STR17R. INSTALLED FRAME REPAIR PER SRM 53-10-4. REPAIR SIZE 19 BY 6.SDR DHL9770387DFrame · crackedD-CHECK, STA 520 ABOVE STR 17R, INBOARD FLANGE OF RIB DENTED AND CRACKED. CUT OUT DAMAGED AREA 4 BY 1.25 PER SRM 53-10-4. INSTALLED FRAME REPAIR AT STA 520 STR17R PER SRM 53-10-4. REPAIR SIZE 14 BY 6.SDR DHL9770386DFrame · crackedD-CHECK, STA 540 ABOVE STR 17R, INBOARD FLANGE OF RIB DENTED AND CRACKED. REMOVED DAMAGED AREA AND INSTALLED FRAME REPAIR AT STA 540, STR 17R PER SRM 53-10-4. REPAIR SIZE 11 BY 6.SDR DHL9770385DFrame · crackedD-CHECK, STA 560, ABOVE STR 17, INBOARD FLANGE OF RIB IS DENTED AND CRACKED. CUTOUT DAMAGED AREA 5 BY 1.5 PER SRM 53-10-4. INSTALLED FRAME REPAIR AT STA 560 ABOVE STR17R PER SRM 53-10-4. REPAIR SIZE 5.5 BY 14.75.SDR DHL9770384DFrame · crackedD-CHECK, STATION 580 ABOVE STR17R, INBOARD FLANGE OF RIB DENTED AND CRACKED. CUTOUT DAMAGED AREA 10 BY 1.5 AT STA 580 ABOVE STR 17R, INBOARD FLANGE OF RIB PER SRM 53-10-1. INSTALLED DOUBLER REPAIR AT BS 580 ABOVE STR 17R PER SRM 53-10-4. DOUBLER REPAIR SIZESDR DHL9770383DFrame · crackedD-CHECK, FUSELAGE FRAME CRACKED AT FASTENER BS804, STR 14R. STOP DRILLED CRACK AND INSTALLED ANGLE REPAIR AT FUSELAGE FRAME 804 STR 14R PER SRM 51-40-3 AND 51-30-2. SIZE OF REPAIR 13 BY 1 BY 1.SDR DHL9770382DFitting · crackedD-CHECK, RT SERVICE DOOR AT BS 660, CORROSION AT AFT UPPER DOOR CUTOUT. REMOVED CORROSION PER SRM 51-10-6. FOUND CRACK ON VISUAL INSPECTION AT LOWER FASTENER OF UPPER DOOR JAMB FITTING. REMOVED AND REPLACED FITTING PER SRM 51-10-1 PAR 4.SDR DHL9770381DFitting · crackedD-CHECK, RT SERVICE DOOR BS 660, CORROSION AT LOWER FORWARD CUTOUT DOOR JAMB FITTING. REMOVED CORROSION AT RT SERVICE DOOR LOWER FORWARD CUTOUT. FOUND CRACK ON VISUAL INSPECTION AT LOWER FASTENER OF DOOR JAMB FITTING. REPLACED DOOR JAMB FITTINGS AT LOWER FOSDR DHL9770380DVertical Beam · crackedD-CHECK, STA 1183, VERTICAL BEAM LBL27 AT W/L 260 HAS CRACK AT CUTOUT. STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED REPAIR AT VERTICAL BEAM BS 1183 LBL 27 PER BOEING DRAWING 65-C33556 AND SB 727-53-0182. N/R 5499SDR DHL9770379DFrame · corrodedD-CHECK, FOUND CORROSION AT TOP OF FLOOR FRAME BS312, LBL 3. REMOVED CORROSION FROM FRAME AT BS 312, LBL3. CUTOUT DAMAGED SECTION, APPROXIMATELY 8 AT TOP OF FLOOR FRAME BS 312 LBL 32 PER SRM 53-10-8. INSTALLED FLOORBEAM REPAIR AS PER SRM 53-10-8 FIG 7. REPSDR DHL9770378DFrame · corrodedD-CHECK, CORROSION ON FLOOR FRAME BS 344, LBL62-RBL62. REMOVED AND REPLACED CABIN FLOOR FRAME BS 344 FROM LBL62 TO RBL62 PER SRM 51-10-1 PAR 4 AND 51-30-2.SDR DHL9770377DSeat Track · corrodedD-CHECK, SEAT TRACK FOUND CORRODED AT BS 344-360, RBL62. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM51-10-1 PAR 4 AND 51-30-2.SDR DHL9770376DSeat Track · corrodedD-CHECK, CORROSION ON SEAT TRACK, BS 380-445, LBL62. REMOVED AND REPLACED SEAT TRACK FROM BS 380-445 AT LBL62.SDR DHL9770375DFrame · crackedD-CHECK, CIRCUMFERENTIAL FRAME HAS 2 CRACKS AT BS 312 STR13R. STOP DRILLED CRACKS PER SRM 51-30-2. INSTALLED FRAME REPAIR PER SRM 53-10-4 FIG 1 7075-0 .080 12 BY 33 BY 4, 7075-O WAS HEAT TREATED TO 7075 T6 PER BAC5602.SDR DHL9770374DSeat Track · corrodedD-CHECK, SEAT TRACK AT BS 480-620 LBL45 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK BS 480-620, LBL 45 PER SRM 53-10-5.SDR DHL9770373DAngle · corrodedD-CHECK, FLOOR WEB AND SEAT TRACK SUPPORT ANGLE AT BS 580-600, LBL45 HAS CORROSION. REMOVED CORROSION ON FLOOR WEB AND SUPPORT ANGLE PER SRM 51-10-06. REMOVED AND REPLACED SEAT TRACK BS 580-600 PER SRM 53-10-5 FIG 1.SDR DHL9770372DAngle · corrodedD-CHECK, FLOOR WEB AND SEAT TRACK SUPPORT ANGLE BS 620-640, LBL45, CORRODED. REMOVED CORROSION ON FLOOR WEB FROM BS 620-640. REPLACED SUPPORT ANGLE SPLICE AT BS 620-640 LBL 45, PER SRM 53-10-5.SDR DHL9770371DSeat Track · corrodedD-CHECK, CORROSION ON SEAT TRACK TOP AND AT HOLES BS 590-630,LBL23. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM BS 590-630, RBL 23 PER SRM 53-10-5 FIG 1.SDR DHL9770370DFrame · corrodedD-CHECK, FLOOR FRAME CORRODED AT TOP AND AT HOLES, BS 680, LBL 62-RBL62. CUTOUT AFFECTED AREA 3 BY 2.25 AT BS 680, LBL 62, PER SRM 53-10-8 FIG 5.SDR DHL9770369DSeat Track · corrodedD-CHECK, SEAT TRACK HAS CORROSION ON TOP AND AT FASTENER HOLES, BS 670-740, RBL62. REMOVED AND REPLACED CABIN SEAT TRACK FROM BS 670-740, RBL 62, PER SRM 53-10-5 FIG 1.SDR DHL9770368DSeat Track · corrodedD-CHECK, SEAT TRACK HAS EVIDENCE OF CORROSION AND BARE METAL EXPOSED, BS 630-740, RBL45. REMOVED AND REPLACED CABIN SEAT TRACK FROM BS 630-740, RBL45, PER SRM 53-10-5 FIG 1.SDR DHL9770367DFrame · crackedD-CHECK, STA 312 RIB CRACKED AT STR 13R. INSTALLED FRAME REPAIR PER B 727 SRM 53-10-4 FIG 1.SDR DHL9770366DTieclip · crackedD-CHECK, STA 440 STR 2L TIE CLIP HAS CRACK. REPLACED TIE CLIP AT STA 440 STR 2L PER B 727 SRM 51-40-3. REPAIR SIZE 3 INCH BY 3 INCH.SDR DHL9770393DTie Clip · crackedAT D-CHECK, FRAME TO STR TIE CLIP CRACKED, FS 1090 STR 7 R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1.SDR DHL9770392DVertical Flange · corrodedAT D-CHECK, WING CENTER SECTION AFT LOWER SPAR HAS CORROSION AND CRACK FROM TOP VERTICAL FLANGE AND POPPED FASTENERS LBL 4 FS 870. REMOVED PREVIOUS WEB REPAIR. REMOVED CORROSION, OUT OF LIMITS, INSTALLED REPAIR PER SRM 51-40-4, 4 BY 16.SDR UPS97223766Skin · crackedINSPECTION TYPE:C, RT WING L/E SKIN CRACKED ABOVE REFUELING PANEL SLAT STN 128 APROX. REPAIR CARRIED OUT I.A.W. SRM 57-30-4 FIG 4.SDR UPS97223573Light · malfunctionedINSPECTION TYPE:N/A, FWD ENTRY DOOR EMERG LIGHT STAYS ON. REPLACED LIGHT ASSY, CHECKS OK (P/N 10-0067-9), (S/N 4249) ON, (S/N UPS1730) OFF.SDR UPS97223773Skin · delaminatedINSPECTION TYPE:C, NR 7 SPOILER PANEL LWR SKIN IS DELAMINATED AT I/B AND IN AREA OF SMALL DOUBLER. NR 7 SPOILER REPAIRED I.A.W. EO C-5100-7322.SDR UPS97223771Skin · delaminatedINSPECTION TYPE:C, LT O/B MIDFLAP T/E IS DELAMINATED IN 3 AREAS ON UPPER AFT SKIN WEDGE. 3 AREAS OF THE LT O/B MIDFLAP T/E WERE REPAIRED I.A.W. EO C-5100-7 322.SDR UPS97223769Web · crackedINSPECTION TYPE:C, CRACK AT FWD WALL OF LT WHEELWELL AT BS 870 LBL 56 AT RIVET. REPAIRED I.A.W. SRM 53-10-9 FIG 4.SDR UPS97223768Stringer · damagedINSPECTION TYPE:C TO AID IN REMOVAL OF STR 8 R END FITTING AT BS 1183. CUT STRINGER BETWEEN BS 1148 AND 1166. STRINGER REPAIRED I.A.W. SRM 53-10-3 FIG 3.SDR UPS97223794Seat Track · corrodedINSPECTION TYPE:C, EVIDENCE OF CORROSION BETWEEN TRACK AND HORIZONTAL MEMBER BS 680 RBL 14. CORRODED BEYOND LIMITS I.A.W. SRM 53-10-1. TRACK REPAIRED IAW SRM 53-10-5 FIG 5.SDR UPS97223779Ramp Skin · wornINSPECTION TYPE:C, NR 3 ENG THRUST REV LOWER DOOR RAMP SKIN WORN DUE TO CHAFFING OF SEAL REPAIRED I.A.W. EFIS AND RE ENGINE SUPP SRM 54-10-03 FIG 203.SDR UPS97223776Ramp Skin · wornINSPECTION TYPE:C, NR 1 ENG T.REV LOWER DOOR INNER RAMP SKIN WORN DUE TO CHAFFING OF SEAL. REPAIR CARRIED OUT I.A.W. EFIS AND RE ENGINE SUPPLEMENT SRM 54-10-0 3 FIG 203.SDR UPS97223775Skin · delaminatedINSPECTION TYPE:C, NR 5 SPOILER PANEL HAS TWO SMALL AREAS OF DELAMINATION ON LWR SKIN AT O/B FWD END AND I/B MIDLE AT EDGE. NR 5 SPOILER PANEL REPAIRED I.A.W. EO C-5100-7322.SDR UPS97223796Skin · delaminatedINSPECTION TYPE:C, NR 1 SPOILER PANEL UPPER FWD I/B END OF PANEL, OLD REPAIR IS DELAMINATED. NR 1 SPOILER PANEL REPAIRED I.A.W EO C-5100-7322.SDR UPS97223795Beam · crackedINSPECTION TYPE:C, CRACK FOUND ON UPPER BEAM OF MAIN CARGO DOOR AT BS 506 APPROX. BEAM REMOVED AND REPLACED IAW BOEING DRAWING NR 65-25337.SDR UPS97223785Skin · crackedINSPECTION TYPE:C, RT WING L/E SKIN CRACKED ABOVE REFUELING PANEL SLAT STN 118 APROX. REPAIR CARRIED OUT I.A.W. SRM 57-30-4 FIG 4.SDR UPS97223781Skin · delaminatedINSPECTION TYPE:C, NR 4 SPOILER PANEL HAS DELAMINATION IN THE AREA OF THE ACTUATOR ROD CUT OUT. NR 14 SPOILER PANEL REPAIRED I.A.W. EO C-5100-7322.SDR UPS97223765Skin · delaminatedINSPECTION TYPE:C, RT WING NR 13 SPOILER HAS DELAM IN AREA OF ACTUATOR ROD CUT-OUT AREA REPAIRED I.A.W. EO -C-5100-7322.SDR UPS97223764Skin · corrodedINSPECTION TYPE:C, SUSPECT CORROSION BETWEEN BS 1160 AND BS 1183 STR 10R. REPAIR TO LAP AT STR 10 R CARRIED OUT BETWEEN BS 1134 AND 1183 I.A.W .EO B727-5330-0509 APPENDIX 8.3 AND SRM 53-30-3 FIG 14SDR UPS97223763Frame · crackedINSPECTION TYPE:C, CRACK BETWEEN FASTENERS BS 740 RT FUSELAGE FRAME BETWEEN STR 18R AND STR 19R. REPAIR CARRIED OUT I.A.W. UPS EO B727-5310-7497 APPENDIX B AND SRS EO 97-15-005 UPS ENGINEERING FILE NUMBER 727-53-1450.SDR DHL9770258DFitting · crackedAT D-CHECK, MAIN CARGO DOOR LATCH SUPPORT FITTING AT FS 520 IS CRACKED ON RADIUS. REMOVED AND INSTALLED NEW FITTING PER SRM 51-10-1.SDR DHL9770259DFitting · crackedAT D-CHECK, RT MID GALLEY DOOR CUTOUT FITTING FOR UPPER HINGE PLATE CRACKED. HFEC, CRACK CONFIRMED. REMOVED AND INSTALLED NEW FITTING PER SRM 51-10-1. INSTALLED NEW STOP PAD PER SRM 51-10-1.SDR DHL9770253DFloorbeam · corrodedAT D-CHECK, CORROSION ON FLOORBEAM STA 303.9 FROM BL 0 TO LBL 10. REPLACED ANGLE FROM BL 0 TO LBL 13 PER SRM 51-30-2, 13 X 1.5 X 1 X1.SDR DHL9770218DFloorbeam · corrodedAT D-CHECK, CORROSION ON FLOORBEAM UPPER CHORD STA 277 FROM LBL 14 TO RBL 14. REMOVED MANUAL EXTENSION DRUM FOR ACCESS, CUT OUT DAMAGED AREA, LBL 3, CUT OUT 1 X 3.5, CUT OUT DAMAGED AREA 7 TO 10, 1 X 3.5. INSTALLED REPAIRS PER SRM 51-40-1.SDR DHL9770217CFloorbeam · corrodedAT D-CHECK, CORROSON ON FLOORBEAM STA 277 LBL 14. REMOVED MANUAL EXTENSION DRUM, CUT OUT CORROSION, INSTALLED REPAIR PER SRM 51-40-1. REINSTALLED EXTENSION DRUM.SDR DHL9770263DAir Stair · corrodedAT D-CHECK, AFT AIRSTAIR FS 1342 RT HORIZONTAL CHORD ATTACH TO VERTICAL REAR SPAR HAS CORROSION. REMOVED CORROSION, OUT OF LIMITS. INSTALLED ANGLE REPAIR PER AVITAS ENGINEERING PMSI 155D-4, ANGLE 7 BY 2 BY 2, N/R 4263.
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