Boeing 727-22
Service difficulty reports · 1,282
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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 = '72722' 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 = '72722' 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 96FDEA01202Skin Panel · gougedNR 0110, 004, BS 380 PLUS 15 WL 160, STR 23 TO 24R THERE IS A SHARP PROTRUDING DENTS IN SKIN. *S/D* REPAIRED DENT AT BS 380 PLUS 15 BETWEEN STR 23 AND 24 RIGHT PER SRM 53-30-3 FIG 3.SDR 96FDEA01201Clip · corrosionDISCREPANCY: NR 0274 (003) GOUGE IN STRING CLIP BS 910 STR 11 RT. ***S/D*** REMOVED STR CLIP AT BS 910, STR 11 RT, AND FOUND GOUGE TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED WITH NEW STRINGER CLIP.SDR 96FDEA01200Floor Beam · corrodedDISCREPANCY: NR 0301 (002) CORROSION (53-113-01-27 ) ON LOWER FLANGE OF FLOORBEAM, BS 1110, BBL 50 TO LBL 30 AT THE NUTPLATE HOLES. ***S/D*** REMOVED CORROSION AND REPAIRED LOWER FLANGE OF FLOOR BEAM AT BS 1110, RBL 50 TO LBL 30, REFERENCE SRM 53-10-8, FIG SDR 96FDEA01199Frame · corrodedNR 0256, 001, CORROSION (C53-111-01) ON FRAME STR 580 BETWEEN STR 22 TO 25 LT FWD BAY 8. *S/D* CORROSION ON FRAME BS 580, BETWEEN STR 22 TO 25 LT IS OUT OF LIMITS PER SRM 53-10-01. REPAIRED FRAME PER SRM 51-40-3, ALODINED AND PRIMED ALL BARE METAL.SDR 96FDEA01194Intercostal · corrodedDISCREPANCY: NR 0563 (007) CORROSION (C53-221-01) ON INTERCOSTAL BS 277-295, LBL 13 WL 208 ***S/D*** REMOVED AND REPLACED UPPER CHORD OF INTERCOSTAL, FLOOR SUPPORT BS 277 TO 295, LBL 13, WL 208. CORROSION FOUND TO BE OUT OF LIMITS.SDR 96FDEA01214Web · corrodedDISCREPANCY: NR 0574 (012) CORROSION (C53-221-01) ON UNDERSIDE OF HORIZONTAL WEB AND L-ANGLES BS 224-259, LBL 42-54, WL 224-236 CORRECTIVE ACTION: REPAIRED HORIZONTAL WEB BS 237 TO 259, LBL 42-54, WL 224-232, AND REPLACED L-ANGLES IAW SRM 51-40-2, DUE TO COSDR 96FDEA01170Lug · corrosionMR 0681 AND NR 039. NR 2 K-FLAP HAS CORROSION AROUND OUTBOARD LUG UPPER BOLT HOLE. ****S/D*** REMOVED CORROSION FROM NR 2 K-FLAP, OUTBOARD LUG UPPER HOLE AND REPAIRED PER FEDEX DRAWING SR 27-57-010, REV B.SDR 96FDEA01169Angle · crackedNR 0405 AND NR 038, AFT CARGO DOOR HAS CRACK INDICATION IN RADIUS OF NR 4 (FROM TOP) OUTBOARD L-ANGLE, 20 INCHES AFT OF FWD EDGE. *****S/D**** COMING.SDR 96FDEA01180Floor Beam · corrosionMAIN CARGO CORROSION ON FLOOR BEAM AT SCREW HOLES FROM LBL 45 - 54, STA 344. REMOVED CORROSION PER SRM 53-10-1. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8 AND EA 7-5310-28760, DATE 6-24-96.SDR 96FDEA01164Bonding Jumper · corrodedNRO0684 AND 037, NR 2 K-FLAP HAS CORROSION AROUND I/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* BLENDED CORROSION AND REPAIRED RIB IAW FEDEX SRM 57-50-3 AND FEDEX DRAWING SR 27-57-010 REV B.SDR 96FDEA01149Floor Beam · corrodedNR0354 AND 036, CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 680 RBL 2 TO 25 WL 208. *S/D* REPAIRED TOP CHORD OF FLOOR BEAM AT BS 680 RBL 2 TO 25 WL 208.1 PER FEDEX SRM 53-10-8 FIG 3.SDR 96FDEA01148Stringer · crackedNR0587 AND 035, WHILE WORKING NRO213 FOUND CRACK AND GOUGE IN STR 4R BS 600 IN U-CHANNEL. *S/D* REMOVED DAMAGE AT BS 600 STR 4R, REPAIRED PER FEDEX SRM 53-10-1 FIG 1.SDR 96FDEA01138Shear Tie · crackedNR 0321 AND NR 034. BS 1070, LBL 51, STR 22L SHEAR TIE IS CRACKED AT FASTENER. ****S/D**** REPAIRED SHEAR TIE AT BS 1070, LBL 51, STR 22L PER FEDEX SRM 53-10-4, FIG 11.SDR 96FDEA01121Beam · corrosionNR 0650 AND 028. CORROSION C53-221-01 ON 25G BEAM STA 268, LBL 2, WL 208. ****S/D**** REMOVED AND REPLACED 25 G-BEAM, STA 268, LB 2, WL 208 PER FEDEX SRM 51-10-1.SDR 96FDEA01120Web · corrosionNR0610 AND 027, CORROSION (C53-224-01) UNDER WEB BETWEEN STA 234 TO 259 WL 227 LBL 48.SDR 96FDEA01118T-Fitting · corrodedNR 0417 AND NR 025. T-FITTING AT BS 360, STR 20L IS CORRODED BEYOND LIMITS. ****S/D**** REMOVED AND REPLACED T-FITTING. REF: FEDEX SRM 51-30-2.SDR 96FDEA01113Chord · crackedNR0545 AND 020, CRACK IN I/B FLANGE OF STR 18A REINFORCEMENT CHORD BS 914.5 RBL 63.7 WL 189. *S/D* REPAIRED CRACK IN I/B FLANGE OF STR 18A REINFORCEMENT CHANNEL BS 914.5 RBL 63.7 WL 189 FEDEX EA 7-5310-29176, FUNCTIONALLY TEST GOOD PER FEDEX MM 32-30-0.SDR CA960627102Rod End · broken(CAN) AIRCRAFT REQUIRES 3 UNITS OF LEFT ROLL TRIM IN ALL PHASES OF FLIGHT. BROKEN ROD END ON #11 SPOILER ACTUATOR. ACTUATOR REPLACED.SDR 96FDEA01105Shear Tie · crackedNR0671 AND 019, FOUND CRACKED SHEAR TIE BS 321 RBL 15 TO 19 WL 148. *S/D* REPAIRED CRACKED FRAME AND SHEAR TIE AT BS 321 RBL 15 TO 19 WL 148 IAW SRM 53-10-4.SDR 96FDEA01104Te Wedge · delaminatedNR 0668 AND NR 018. L/W I/B MID FLAP LWR O/B T/E WEDGE DELAMINATED. ****S/D**** REPAIRED L/W I/B MID FLAP IAW FEDEX SRM 51-40-6.SDR 96FDEA01103Shear Tie · crackedNR0646 AND 017, WHILE WORKING NR0348 AFTER REMOVING R/LOWER NOSE CHORD, FOUND CRACKED AND CORRODED SHEAR TIE AT BS 328 WL 148 RBL 15 TO 18. *S/D* REMOVED DAMAGED SHEAR TIE AT BS 328 WL 148 RBL 15 TO 18 IAW FED EX SRM 53-10-4.SDR 96FDEA01102Frame · dentedNR0494 AND 016, DENT IN FRAME AT BS 660 LBL 39 WL 162. *S/D* REPAIRED FRAME AT BS 660 LBL 39 WL 162 AS PER FED EX SRM 51-40-3.SDR 96FDEA01101Frame · dentedNR0499 AND 015, DENT IN FRAME AT BS 620 RBL 39 WL 162. *S/D* REMOVED DENT IN FRAME AT BS 620 RBL 39 WL 162. FABRICATED REPAIR PARTS AND INSTALLED PER FED EX SRM 51-40-3.SDR 96FDEA01100Floor Beam · gougedNR0481 AND 014, FOUND GOUGE IN FLOOR BEAM STA 560 RBL 6 WL 198, FWD BAY. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8.SDR 96FDEA01099Floor Beam · corrodedNR0477 AND 011, CORROSION (C53-111-01, -2) ON FLOOR BEAM STA 600 RBL 2, 8, 13, 15, 18 WL 198, FWD BAY. *S/D* BLENDED AND INSTALLED REPAIR STRAP IAW FED SRM 53-10-1 AND 53-10-8.SDR 96FDEA01098Fitting · corrodedNR 5 K-FLAP CENTER HINGE FITTING THAT ATTACHES TO FIXED L/E CORRODED. REMOVED AND REPLACED PER SRM.SDR 96FDEA01097Fitting · corrodedNR 1 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED. REMOVED AND REPLACED PER SRM.SDR 96FDEA01096Fitting · corrodedNR0376 AND 008, NR 2 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED (C57-562-01). *S/D* REMOVED AND REPLACED NR 2 K-FLAP TO LEADING EDGE MOUNT FITTING FOR THE CENTER HINGE IAW SRM 51-30-2.SDR 96FDEA01095Clip · gougedNR0212 AND 007, DAMAGED RIVETS AND STR CLIP AT BS 720 STR 4R. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 720, STR 4 RT PER SRM 53-10-8.SDR 96FDEA01094Clip · gougedNR0211 AND 006, MISSING FASTENERS FROM STR CLIP AT BS 660 STR 3R AND DAMAGED STR CLIP. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 660, STR 3 RT PER SRM 53-10-8.SDR 96FDEA01093Clip · gougedNR0210 AND 005, DAMAGED STR CLIP AT BS 660 STRS 4R. *S/D* REMOVED DAMAGED CLIP AND INSTALLED NEW STRINGER CLIP AT BS 660 STR 4 RT PER SRM 53-10-8.SDR 96FDEA01092Floor Beam · corrodedNR0352 AND 004, CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 600 RBL 10 TO 47 WL 208. *S/D* REMOVED CORROSION ON FLOOR BEAM TOP CHORD BS 600 RBL 10 TO 47 WL 208. FOUND AREA AT RBL 10 TO 17 TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM IAW SRM 53-10-08.SDR 96FDEA01081Web · corrosionNR 0624 (013) CORROSION (C53-221-01) UNDER WEB BETWEEN STA 219.8 TO 227.8, WL 227, LBL 43.SDR 96FDEA01080Floor Beam · double holeNR 0514, 012 DOUBLE HOLE IN FLOOR BEAM TOP CHORD BS 1110, LBL 32, WL 208. *S/D* TRIMMED OUT DOUBLE HOLE IN FLOOR BEAM TO CHORD BS 1110 LB 32 WL 208. FABRICATED REPAIR ANGLES AND FILLER, ALODINED AND PRIMED FLOOR BEAM AND REPAIR ANGLES, INSTALLED PARTS PER FSDR 96FDEA01079Floor Beam · corrosionNR 0353, 003 CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 620, LBL 10 TO 21 AND RBL 2 TO 56 WL 208. *S/D* REPAIRED BS 620 FLOOR BEAM UPPER CHORD LBL 21 TO RBL 56 IAW FEDEX SRM 53-10-8.SDR 96FDEA01078Skin · delaminationNR 0324, 003 DELAMINATION ON R/W O/B AFT FLAP ABOUT 5 INCHES FROM I/B END. *S/D* REPAIRED DELAMINATION ON R/W O/B AFT FLAP 5 INCHES FROM I/B END IAW FEDEX SRM 51-40-06 FIG 40.SDR 96FDEA01077Fore Flap · delaminationDELAMINATION ON R/W I/B FORE FLAP UPPER SURFACE ABOVE CENTER TRACK. *S/D* REPAIRED R/W I/B FORE FLAP UPPER SURFACE ABOVE CENTER TRACK IAW FEDEX SRM 51-40-6 FIG 36.SDR 96FDEA01076Skin · delaminationNR 0322, 001 DELAMINATION ON R/W I/B FLAP UPPER SURFACE 48 INCHES FROM I/B END. *S/D* REPAIRED DELAMINATION ON R/W I/B AFT FLAP UPPER SURFACE 48 INCHES FROM I/B END IAW FEDEX SRM 51-40-06, FIG 40 PG 75.SDR 96FDEA01075Support Beam · corrosionNR 0647, (002) WHILE WORKING NR0348 AFTER REMOVING RT LWR NOSE CHORD FOUND DRAG BRACE SUPPORT BEAM TO BE CORRODED OUT OF LIMITS PER SRM AT BS 328 TO 345 WL 148 RBL 15. *S/D* REMOVED AND REPLACED DRAG BRACE SUPPORT T-BEAM AT BS 328 TO 345 WL 148 RBL 15, INSTALSDR 96FDEA01074Floor Beam · corrosionNR 0548, (001) WHILE WORKING NR0283 FOUND CORROSION ON UPPER SURFACE OF 480 FLOOR BEAM RBL 45. *S/D* REPAIRED FLOOR BEAM BS 480 RBL 45 IAW SRM 53-10-8.SDR 96FDEA01052Door Switch · failedAT FLT LEVEL 310, MCD ANNUNCIATOR LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST AND DEPRESSURIZED A/C IN DESCENT. LIGHT REMAINED ILLUMINATED UNTIL 2,000 FEET ABOVE GROUND LEVEL ON APPROACH, THEN WENT OUT. NO OTHER SYMPTOMS WERE NOTED, NO NOISE OR LOSS OF PRESSUSDR 96FDEA00733Strap · misdrilledWHILE WORKING 7-5310-7-3367B PT9, DISCOVERED FASTENER HOLES INTERFERED WITH RADIUS OF ANGLE AT BS 825.95 WL 207 TO 198 LBL 65, DUE TO INSTALLATION OF REPAIR STRAP. REPAIRED STRAP BS 825.95 WL 207 TO 198 LBL 65 PER FEDEX EA 7-5310-28184.SDR 96FDEA00732Web · corrosionUPON REMOVAL OF PRESSURE PAN, FOUND CORROSION ON WEB BS 760.95 WL 207 LBL 65 TO 68. REPAIRED BS 760.95 WEB WL 207 LBL 65-68 PER FEDEX EA 7-5310-28183.SDR 96FDEA00724Stringer · corrodedCORROSION (C53-113-01, 2) ON STR 27R AT BS 990 RBL 22 WL 142. INSTALLED STR SPLICE REPAIR PER SRM 53-10-3.SDR 96FDEA00720Hydraulic Module · leakingMAIN GEAR AND USED ALT FLAP EXT IN FLT AND BOTH A-SYS LOW PRESS LIGHT CAME ON, FOLLOWED BY OVERHEAT TO SYS. OVERHEAT LIGHT WENT OUT, BUT HAD A-SYS PRESS WITH GOOD A-SYS QTY. RED TAB PROCEDURE AND EWR MX SUGGESTIONS, DID NOT REGAIN A-SYS PRESS. NOTE - IN RIC SDR 96FDEA00719Strut · reqd serviceNOSE GEAR DOORS WOULD NOT RETRACT ON TAKEOFF. RECYCLED THE GEAR AND TRIED AGAIN, STILL NO GEAR DOORS RETRACTED. WE OBSERVED AIR SPEED LIMITS, LIGHT EXTINGUISHED EN ROUTE. FOUND NOSE STRUT DEFLATED. RESEALED UPPER GLAND NUT PER MM 32-21-1 AND SERVICED SAME,SDR 96FDEA00727Vertical Web · corrodedCORROSION (C53-113-01, 2) ON AFT BAY WEB SILL BS 1057 TO 1110 RBL 21 WL 148.5. FOUND UPON REMOVAL OF STRAP NR 0217. REMOVED AND REPLACED AFT BAY WEB SILL FROM BS 1057 TO 1110 RBL 21 WL 148.5.SDR 96FDEA00726Door Frame · corrosionCORROSION (C53-113-01, 2) ON DOOR FRAME AT BS 1057 RBL 30 WL 148 AT NUTPLATE HOLES. REPAIRED DAMAGE PER SRM 51-40-3.SDR 96FDEA00725Keel Beam · corrosionCORROSION (C53-113-01, 2) ON RT KEEL BEAM RBL 6 WL 140 BS 1020, 1030, 1042, 1056 AND 1085. REPAIRED KEEL BEAM IAW FEDEX EA 7-5310-28083.SDR 96FDEA00721Strap · corrodedWHILE WORKING EO 7-5310-7-3367B, FOUND REINFORCEMENT STRAP AND T-CLIP TO BE BADLY CORRODED AT BS 760 WL 206 LBL 70.5. REMOVED AND REPLACED STRAP AND CLIP AT BS 760 WL 206 LBL 70.5.
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