Boeing 727-2A1
Service difficulty reports · 502
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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 = '7272A1' 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 = '7272A1' 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 FOTR20006NR5753Angle · corrodedSTA 1166 AT STR 17 WEB AREA CORRODED. REPAIRED ON FASI W/O NR 20006, N/R 005753. REMOVED AND REPLACED UPPER ANGLE AND LOWER CHANNEL SUPPORT AT STA 1166, STR 17R IAW B727 SRM 53-10-1-FIG. 1, 51-20-1 AND 53-10-2, REV 102. MATERIAL USED: CHANNEL; 7075-T6, 0.08SDR FOTR20006NR 5760Floorbeam · damagedSTA 1070 FLOORBEAM DOUBLE DRILLED HOLE RBL.50. REPAIRED ON FASI W/O NR 20006, N/R 04858. REMOVED AND REPLACED UPPER SUPPORT FITTING AT RT LOWER TORQUE BOX WEB AT VENTRAL STAIRS STA 1263 WITH P/N 65C27137-1 IAW B727 SRM 53-10-2, REV 102.SDR FOTR20006NR1842Frame · dentedMAIN CABIN FRAME BS 280 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/ONR 20006, NR 01842. INTALLED REPAIR DOUBLER TO FRAME AT BS 380, STR 6R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TSDR FOTR20006NR1841Frame · dentedMAIN CABIN FRAME BS.400 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/O 20006,NR 01841 INSTALLED REPAIR DOUBLER TO FRAME AT BS 400, STR 6R, DUE TO DENT, IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDISDR FOTR20006NR1798Intercostal · crackedAFT PIT HAS A CRACK AT INTERCOSTAL STR 23L BETWEEN BS 950D TO 950E. REPAIRED ON FASI W/O NR20006, NR01798. R & R CRACKED INTERCOSTAL BETWEEN BS 950D TO BS 950E, STR 23L IAW SRM 51-20-1 FIG 1 REV 102 AND DWG NR 65-56125. MATERIAL USED: 7075-T6, DIM.; 19.5 X 4 SDR FOTR20006NR1795Skin · crackedLT OTBD FOREFLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O NR 20006,NR 01795 - INSTALLED REPAIR DOUBLER TO LT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-4 FIG 7 REV 102. MATERIAL USED: 2024-T3, DIM.; 6 X 4 X 0.063.SDR FOTR20006NR1794Skin · crackedRT OTBD FORE FLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O 20006, NR 01794. INSTALLED REPAIR DOUBLER TO RT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-2, FIG 4 AND 57-50-4 FIG 1 REV 102. MATERIAL USED: 2024-T3, DIM.; 5 X 3 X 0.063.SDR FOTR20006NR1778Skin · delaminatedRT OTBD AILERON T/E WEDGE PUNCTURED ON LOWER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 01778 - INSTALLED HOT BONDED REPAIR DOUBLER TO RT OTBD AILERON TAB IAW SRM 51-40-20 PARA 7, 20 AND 22, REV 102. MATERIAL USED: 2024-T3, 0.012” THICK, DIM.; 3 X 3. CALCULATSDR FOTR20006NR5683Panel · delaminatedNR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING IS DISBONDED. REPAIRED ON FASI WO 20006, N/R 05683. INSTALLED BONDED REPAIR TO NR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING AT WBL 110 IAW B727 SRM 51-40-20. MATERIASDR FOTR20006NR5666Skin · delaminatedLT INBD AILERON TAB HAS DELAMINATION LOWER SURFACE CENTER. REPAIRED ON FASI WO 20006, N/R 05666. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 275 IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012, DIM: 7.SDR FOTR20006NR5665Skin · delaminatedLT IB AILERON TAB LOWER SURFACE OTBD HAS DELAMINATION AREA-MARKED. REPAIRED ON FASI WO 20006. N/R 05665- INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 295 IAW SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012", DIM: SDR FOTR20006NR5664Skin · delaminatedLT INBD AILERON TAB LOWER SURFACE INBD HAS DELAMINATION. REPAIRED ON FASI WO 20006, N/R 05664. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 250 BY IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012, DIM: 1SDR FOTR20006NR5661Skin · crackedFUSELAGE STA 1096 AT STRINGER 1 FIRST FAIRING FASTENER RT SKIN HAS CRACKS. REPAIRED ON FASI WO 20006, N/R 05661. REPAIRED FUSELAGE SKIN AT STA 1096, STR 1 IAW BOEING S/B 727-53A0204 REV 3. MATERIAL USED: 2024-T3, 0.063, DIM: 13.50 BY 11.25. CUT OUT DIM: 3.SDR FOTR20006NR5649Stringer Clip · gougedSTR TIE CLIP GOUGED STA 440 STR 4R. REPAIRED ON FASI WO 20006, N/R 05649. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 4R, STA 440 IAW BOEING DWG 65-45313 REV E AND B727 SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032, DIM: 3.60 BY 1.80.SDR FOTR20006NR5647Stringer Clip · crackedSTR TIE CLIP CRACK STA 460 STR 2R. REPAIRED ON FASI WO 20006 N/R 05647. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 2R, STA 460 IAW BOEING DWG 65-45313 REV E AND B727 SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032, DIM: 3.60 BY 1.80.SDR FOTR20006NR5633Stringer Clip · crackedCABIN AREA STA 700, STRINGER 7L FRAME TO STRINGER BRACKET IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05633- R & R STRINGER TO FRAME CLIP AT STR 7L, STA 700 IAW DWG 65-45313 REV E AND SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032", DIM: 3.60" X 1.80".SDR FOTR20006NR5630Stringer · crackedCABIN AREA STA 720B FWD OF LIGHT HOUSING, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05630- REPAIRED STR 15L AT STA 720B IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: ANGLE; 7075-T6, 0.040", DIM: 6.0".SDR FOTR20006NR5629Stringer · crackedCABIN AREA STA 720C AFT OF LIGHT HSG, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO20006. N/R 05629- REPAIRED STR 15L AT STA 720C IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: CHANNEL; 7075-T6, 0.040", DIM: 6.0" X 0.750", RADIUS FILLER; 7075-T6, 0.080", DISDR FOTR20006NR5443Frame · puncturedAFT PIT FRAME PUNCTURED STR 27L BS 1130. REPAIRED ON FASI WO 20006, N/R 05443. REPAIRED AFT CARGO COMPARTMENT FRAME AT STR 27L, STA 1130 IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: ANGLE DOUBLER; 7075-T6, 0.063, DIM: 12.25 BY 4.125SDR FOTR20006NR5442Shear Tie · corrodedAFT PIT FRAME SHEAR TIE HAS SURFACE CORROSION BETWEEN STR 30 AND 28R. REPAIRED ON FASI WO 20006, N/R 05442. REMOVED AND REPLACED AFT CARGO COMPARTMENT FRAME SHEAR TIE AND DRAIN MAST SUPPORT CHANNEL AT STA 1148 BETWEEN STR 28R AND STR 30 IAW B727 SRM 53-10-4 SDR FOTR20006NR5604Frame · dentedFWD CARGO COPT FRAME 720A HAS 2 DENTS IN THE UPPER FLANGE BETWEEN STR 24L-25L. REPAIRED ON FASI WO20006. N/R 05604- REPAIRED FRAME AT STA 720A BETWEEN STR 24L AND 25L IAW SRM 51-30-2 AND 51-40-3 FIG. 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050", DIM: 3SDR FOTR20006NR5600Frame · dentedFWD CARGO COMPT FRAME BS 680 UPPER FLANGE IS DENTED AND WEB IS BENT BETWEEN STR 23L-24L. REPAIRED ON FASI WO20006. N/R 05600- REPAIRED FRAME AT STA 680 BETWEEN STR 23L AND 24L IAW B727 SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 70SDR FOTR20006NR5599Frame · dentedFWD CARGO COMPT FRAME BS 680 HAS 4 DENTS IN THE UPPER FLANGE BETWEEN STR 23R-25R, WEB IS BENT. REPAIRED ON FASI WO20006, N/R 05599. REPAIRED FRAME AT STA 680 BETWEEN STR 23R AND 25R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLSDR FOTR20006NR5598Frame · dentedFWD CARGO COMPT FRAME BS 660 HAS 4 DENTS IN THE UPPER FLANGE BETWEEN STR 23R-25R. REPAIRED ON FASI WO20006, N/R 05598. REPAIRED FRAME AT STA 660 BETWEEN STR 23R AND 25R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, SDR FOTR20006NR5586Frame · dentedFWD CARGO COMPT, FRAME BS 520 HAS 2 DENTS IN UPPER FLANGE ABOVE STR 24R. REPAIRED ON FASI WO20006, N/R 05586. REPAIRED FRAME AT STA 520 BETWEEN STR 23R AND 24R IAW B727 SRM 51-30-5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050, DIM: 13.SDR FOTR20006NR5585Frame · dentedFWD CARGO COMPT FRAME BS 500 HAS DENT IN UPPER FLANGE ABOVE STR 23R. REPAIRED ON FASI WO20006, N/R 05585. REPAIRED FRAME AT STA 500 BETWEEN STR 22R AND 23R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 9SDR FOTR20006NR5562Frame · dentedAFT PIT FRAME DENTED AT BS 1030 JUST ABOVE STR 27L. REPAIRED ON FASI WO20006 N/R 05562. REPAIRED FRAME AT STA 1030 BETWEEN STR 26L AND 27L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 11.50 BY 4.20. CUSDR FOTR20006NR5554Frame · dentedAFT PIT FRAME IS DENTED AT BS 950C BETWEEN ST 25L-26L. REPAIRED ON FASI WO20006, N/R 05554. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950C BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.06SDR FOTR20006NR5548Frame · damagedSTA 970 FRAME DOUBLER DRILLED BELOW STR 7R. REPAIRED ON FASI WO20006 N/R 05548. REPAIRED FRAME AT STA 970 BETWEEN STR 7R AND 8R IAW B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: 8.0 BY 3.375. CUT OUT DIM: 1SDR FOTR20006NR5542Frame · damagedSTA 950F RIVET HEAD NOT FLUSH STR 7R, REPAIRED ON FASI WO20006, N/R 05542. REPAIRED FRAME AT STA 950F STR 7R IAW B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071, DIM: 11.750 BY 3.50, FILLER; 7075-T6, 0.071, DIM: 2.75SDR FOTR20006NR5501Frame · damagedMISDRILLED HOLE ON UPPER FLANGE OF BS 1070 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05501. REPAIRED FRAME AT STA 1070 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, SDR FOTR20006NR5500Frame · damaged2 MISDRILLED HOLES ON UPPER FLANGE OF BS 1090 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05500. REPAIRED FRAME AT STA 1090 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.06SDR FOTR20006NR5499Frame · damaged2 MISDRILLED HOLES ON UPPER FLANGE OF BS 1110 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05499. REPAIRED FRAME AT STA 1110 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.06SDR FOTR20006NR5498Frame · damagedMISDRILLED HOLE ON UPPER FLANGE OF BS 1130 FRAME BETWEEN STR 27R-28R. REPAIRED ON FASI WO NR 20006, N/R 05498. REPAIRED FRAME AT STA 1130 BETWEEN STR 27R AND 28R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, SDR FOTR20006NR5495Frame · damagedMISDRILLED HOLE ON UPPER FLANGE OF BS 1050 FRAME BETWEEN STR 27L-28L. REPAIRED ON FASI WO NR 20006, N/R 05495. REPAIRED FRAME AT STA 1050 BETWEEN STR 27L AND 28L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, SDR FOTR20006NR5460Frame · dentedAFT PIT FRAME BS 1090 IS DENTED, JUST ABOVE STR 26L. REPAIRED ON FASI WO NR 20006 N/R 05460. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 1090 BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.SDR FOTR20006NR5458Frame · dentedAFT PIT HAS FRAME DENTED AT BS 1010 BETWEEN STR 26L AND 25L. REPAIRED ON FASI WO NR 20006 N/R 05458. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 1010 BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075SDR FOTR20006NR5457Frame · dentedAFT PIT HAS FRAME DENTED AT BS 970 BETWEEN STR 26L AND 25L. REPAIRED ON FASI WO NR 20006, N/R 05457. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 970 BETWEEN STR 25L AND 26L IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER; 7075-SDR FOTR20006NR5451Frame · dentedAFT PIT RT FRAME BS 950C IS DENTED, BETWEEN STR 26R AND SR 25R. REPAIRED ON FASI W/O NR 20006, N/R 05451. REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950C BETWEEN STR 25R AND 26R IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBLER;SDR FOTR20006NR5450Frame · dentedUPPER FLANGE OF AFT PIT FRAME DENTED AT BS950F STR 25L-27L. REPAIRED ON FASI W/O 20006 REPAIRED AFT CARGO COMPARTMENT FRAME AT STA 950F BETWEEN STR 25L AND 27L IAW SRM 53-10-2 FIG. 5 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 7075-T6, 0.063, DIM: SDR FOTR20006NR5340Skin · delaminatedRT WING INBD AILERON TAB UPPER SURFACE OTBD EDGE IS DELAMINATED. REPAIRED ON ASI WO 20006, N/R 05340. REPAIRED RT WING INBD AILERON TAB UPPER SURFACE AT WBL 295.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLERS; 2024-T3, 0.012,SDR FOTR20006NR5267Skin · punctured(FOTR) RT ELEVATOR UPPER SKIN PUNCTURED AT ELEV STA 67. REPAIRED ON FASI W/O NR 20006, 05267- REPAIRED RT ELEVATOR UPPER SKIN AT ELEV STA 67 IAW SRM 55-20-3 FIG, 4 AND 55-20-2 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.032", DIM: 4.625" X 4.125". CUSDR FOTR20006NR5097Skin · gougedRT ELEVATOR UPPER SKIN GOUGED AT ELEVATOR STA 118. REPAIRED ON FASI WO 20006, N/R 05097- REPAIRED RT ELEVATOR UPPER SKIN AT ELEV STA 118 IAW SRM 55-20-3 FIG, 4 AND 55-20-2 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.032", DIM: 7.375" X 4.125", FILLER; 2SDR FOTR20006NR5306Hinge Bracket · crackedRT WING NR 14 SPOILER OTBD HINGE BRACKET IS CRACKED. REPAIRED ON FASI WO 2000. N/R 05306- R & R RT WING NR 14 SPOILER HINGE BRACKET IAW SRM 51-20-1 FIG 7, REV 102 AND DWG 65-21657 REV E MATERIAL USED: 7075-T6, 0.080", DIM: 4.0" X 3.0".SDR FOTR20006NR5287Skin · chafedLT WING STA 574 UPPER LE SURFACE HAS A DEEPLY CHAFED AREA 13" IN LENGTH. REPAIRED ON FASI WO 20006. N/R 05287- REPAIRED LT WING UPPER L/E SURFACE AT STA 574 IAW SRM 57-30-4 FIG 4, REV 102 MATERIAL USED: DOUBLER; 2024-T3, 0.050", DIM: 10.90", 4.10". FILLER; 20SDR FOTR20006NR5289Skin · crackedLT WING, STA 549, UPPER L/E SLAT TRACK CUTOUT IS CRACKED IN UPPER RADIUS. REPAIRED ON FASI WO 20006. N/R 05289- REPAIRED LT WING UPPER L/E SLAT TRACK CUTOUT AT WS 549 IAW SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 9.50" X 10.0SDR FOTR20006NR5293Skin · crackedLT WING STA 474 SLAT TRACK CUTOUT UPPER L/E CUTOUT IS CRACKED IN THE RADIUS. REPAIRED ON FASI WO 20006, N/R 05293. REPAIRED LT WING LEADING EDGE AT SLAT TRACK CUTOUT AT WS 474 IAW B727 SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER- 2024-T3, 0.063, DIMSDR FOTR20006NR5307Skin · delaminatedRT WING NR 9 SPOILER T/E IS DELAMINATED. REPAIRED ON FASI WO 20006. N/R 05307- INSTALLED BONDED REPAIR DOUBLER TO RT WING NR 9 SPOILER T/E AT WBL 130.0 IAW SRM 51-40-20, REV 102. MATERIAL USED: FILLER; 7075-T6, 0.020", DIM: 2.0" X 50.0", DOUBLER; 7075-T6, 0.SDR FOTR20006NR5351Skin · crackedNR 11 SPOILER 2ND HINGE CUTOUT IS CRACKED AT WS 460. REPAIRED ON FASI WO 20006. N/R 05351- REPAIRED NR11 SPOILER 2ND HINGE CUTOUT AT WS 460 IAW SRM 57-30-4 FIG 10, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071", DIM: 6.0" X 4.50".SDR FOTR20006NR5352Skin Panel · crackedNR 11 SPOILER 3RD HINGE CUTOUT IS CRACKED AT WS 466. REPAIRED ON FASI WO 20006, N/R 05352. REPAIRED NR 11 SPOILER 3RD HINGE CUTOUT AT WS 466 IAW B727 SRM 57-30-4 FIG 10, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071, DIM: 6.0 BY 4.50.
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