Boeing 727-21C

Service difficulty reports · 217

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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 = '72721C'
  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.

SDR 97FDEA00804Clip · crackedNR 0191 051 CRACKED STRINGER CLIPS (2EA) AT BS 1030 6R AND 8R. *** S/D *** REMOVED AND REPLACED STRINGER CLIPS AT BS 1030, STR 6 AND 8 R/H. IAW FED-EX SRM 51-10-1 AND FED-EX SRM 51-30-2.Nov 3, 1997 · N143FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00724Skin · corrodedBULGE IN SKIN LAP AT STR 20, BS 1070 LEFT HAND SIDE. *S/D* REMOVED CORROSION AND REPAIRED SKIN LAP AT STR 20 LEFT HAND BS 1070 PER FED-EX SRM 53-30-3 FIG 14.Oct 10, 1997 · N144FE · Boeing 72721C · Fuselage Main, Plate/SkinSDR 97FDEA00717Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM AT BS 312, LBL 30, WL 208. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORROSION AT BS 312 FLOORBEAM UPPER CHORD LBL 30, WL 208 IAW FED-EX SRM 53-10-8 FED-EX SRM 53-10-1.Oct 9, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00704Skin · corrodedWHILE WORKING NR0768, DISCOVERED CORROSION ON UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190. *S/D* REMOVED CORROSION ON LOWER SURFACE OF UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190 AND REPAIRED PER FED-EX Oct 6, 1997 · N144FE · Boeing 72721C · Fuselage Main, Plate/SkinSDR 97FDEA00698Fitting · crackedNR 0835 050 UPON REMOVAL OF UPPER SPLICE FITTING FOR ACCESS FOR NR 0822, CORROSION ON BOTTLE PIN CASTING, FOUND FITTING TO BE CRACKED BS 876, WL 178 RT SIDE P/N 65-18595-1. REMOVED DAMAGED SPLICE FITTING, UPPER RT SIDE AT BS 876, WL 178, RBL 68-72. BACK DRILOct 1, 1997 · N143FE · Boeing 72721C · Wing, Fuselage Attach FittingsSDR 97FDEA00697Chord · crackedNR 0706 036 STA-PAE - CORROSION (C53-224-05) CRACK IN RT 70.85 PLUS CHORD IS CRACKED ON UPPER VERTICAL FLANGE IN RADIUS FROM BS 760 TO 770, WL 201, RBL 70.5 LONG CRACK REPAIR REQUIRED PER S/B 727-57-0112 REV 5. REPAIRED CRACK IN RT 70.8 PLUS CHORD PER EA 7-5Oct 1, 1997 · N144FE · Boeing 72721C · Wing Miscellaneous StructureSDR 97FDEA00684Floorbeam · crackedNR 0857 035 WHILE WORKING NR 0822 DISCOVERED BS 328 FLOORBEAM WEB TO BE CRACKED T LBL 30, WL 206. REPAIRED BS 328 FLOORBEAM WEB AT LBL 30, WL 206 AS PER FED-EX SRM 51-40-2.Sep 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00683Floorbeam · corrodedNR 0534 034 CORROSION (C53-224-06) AROUND FASTENERS IN THE CARGO TIE DOWN PUCK ON THE BOTTOM OF UPPER FLOORBEAM CHORD AT BS 620, RBL 62.5. REPAIRED UPPER FLOORBEAM CHORD AT BS 620, RBL 15 TO RBL 70 AS PER FED SRM 53-10-8.Sep 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00672Casting · corrodedNR 0794 049 CORROSION (C53-224-02) ON CARGO NET CASTING BS 360 TO 380 IN WALL OF CASTING UNDER NET TIE DOWN LBL 40-45, WL 208 AND RBL 45. REMOVED AND REPLACED CARGO NET CASTING BS 360 TO 380, LBL 40-45 IAW FED-EX SRM 51-30-2. CASTING AT BS 360 TO 380, RBL 40Sep 19, 1997 · N143FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00667Stringer · corrodedNR 0800 048 CORROSION (C53-224-02) ON STRINGER 3, BS 540-560 RT. REMOVED AND REPLACED CORRODED STRINGER WITH A NEW ONE AT BS 490-570 S3R IAW FED SRM 53-10-03.Sep 19, 1997 · N143FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00666Casting · corrodedCORROSION (C53-224-06) IN FORWARD POCKET OF THE BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208. *S/D* REMOVED AND REPLACED BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208 PER FED-EX SRM 51-30-2. ALODINED AND PRIMED PER FED-EX SSep 18, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00665Stringer · crackedNR 0855 WHILE WORKING NR 0630 FOUND STRINGER 26L TO BE CRACKED AT BS 559.5. WHILE INVESTIGATING CRACK ON S26L BS 559.5, FOUND CORROSION IN MANY AREAS. CORROSION PENETRATED MATERIAL THICKNESS MORE THAN 10 PERCENT OF AREA OUT OF LIMITS. PER FED SRM 53-10-1. Sep 18, 1997 · N143FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR UPS97224438Hose · leakingINSPECTION TYPE-N/A, LOSS OF HYDRAULIC SYSTEM 'B' FLUID AT 15,000 FT BOTH 1 AND 2 'B' PUMPS LOW PRESS LIGHTS CAME ON, QTY INDICATION 0. DECLARED EMERGENCY, COMPLIED WITH CHECKLISTS, LANDED WITHOUT FURTHER INCIDENT. FOUND NR 1 'B' PUMP PRESSURE LINE CHAFED THSep 16, 1997 · N934UP · Boeing 72721C · Hydraulic System, MainSDR 97FDEA00653Skin · corrodedNR 0832 032 CORROSION (C53-224-05) ON WING CENTER TANK UPPER SKIN LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5. REMOVED CORROSION ON WING CENTER TANK UPPER SKIN, TOP SURFACE AT LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5 AND REPAIRED PER FESep 12, 1997 · N144FE · Boeing 72721C · Wing, Plate/SkinSDR 97FDEA00650Fitting · corrodedNR 0839 031 CORROSION ON HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45. REMOVED AND REPLACED HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45 AS PER FED-EX SRM 51-10-2, 51-10-1, 51-30-2 AND M/M 51-20-151.Sep 11, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00633Stringer · corrodedCORROSION (C53-224-02) ON LT STRINGER NR 7, BS 680 TO BS 682 AND BS 700 TO BS 702. *S/D* REMOVED CORROSION ON LT STR 7, BS 680 TO 682, 700 TO 702. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED STR 7L IAW FED-EX SRM 53-10-3.Sep 4, 1997 · N143FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00629Fitting · crackedNR 0764 030 FOUND CRACK ON OUTBOARD HOLE OF STRINGER 29R, BS 1103. REMOVED CRACKED STRINGER FITTING. REPLACED WITH A NEW STRINGER FITTING AT BS 1183, STR 29R, IAW FED-EX SRM 51-30-02.Sep 4, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00626Frame · corrodedNR 0628 045 CORROSION (C53-111-01) ON FRAME AT BS 540, STR 26L. REPAIRED FRAME BS 540, STR 26L PER FED-EX SRM 51-40-3 AND 51-10-1.Sep 3, 1997 · N143FE · Boeing 72721C · Fuselage Main, FrameSDR 97FDEA00625Stringer · corrodedNR 0138 044 CORROSION (C53-224-01(3)) ON STRINGER 1 FROM BS 950 TO 1010. REMOVED AND REPLACED STRINGER NR 1 FROM BS 950-1020 PER FED-EX SRM 53-10-3.Sep 3, 1997 · N143FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00618Floorbeam · corrodedNR 0822 028 CORROSION (C53-224-06) ON UPPER SURFACE OF TOP CHORD OF FLOORBEAM BS 328, LBL 29-32, WL 208. REPAIRED TOP CHORD OF FLOORBEAM BS 328 FROM LBL 9 TO LBL 63, WL 208 IAW FED-EX SRM 53-10-8.Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00617Stringer · corrodedNR 0551 029 CORROSION (C53-224-06) ON STRINGER 9 LEFT IN SEVERAL AREAS BETWEEN BS 620 AND 740. REPAIRED 59L BETWEEN BS 620-740 IAW FED 53-10-1 AND FED SRM 53-10-3.Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00612Strap · corrodedCORROSION (C53-111-01,3) ON CENTER STABILIZER STRAP FROM BS 988 TO BS 1090, BL 0 WL 200. *S/D* REMOVED AND REPLACED BL 0 BS 950 TO 1158, WL 200 STABILIZER STRAP PER FED-EX SRM 51-10-1 AD 51-30-2.Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00601Floorbeam · corrodedNR 0840 020 STA-PAE - WHILE WORKING NR0374 FOUND DOUBLE HOLES IN UPPER SIDE OF BS 1130 CHORD, BS 1130, RBL 32 AND 37, LBL 33 AND 38, WL 208 ALSO CORROSION AND CRACK INDICATION AT LBL 33. REPAIRED UPPER CHORD OF 1130 BEAM IAW FED-EX EA 7-5310-36165 AND EA 7-5Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00619Spar Chord · corrodedNR 0748 027 STA-PAE - CORROSION (C57-174-01) ON BS 870 REAR SPAR UPPER CHORD RBL 20-60, LBL 10-40, WL 178. BLENDED, REMOVED CORROSION ON UPPER REAR SPAR CHORD, BS 870, RBL 20-60, LBL 10-40, WL 178. CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. RESep 1, 1997 · N144FE · Boeing 72721C · Wing SparSDR 97FDEA00616Strap · corrodedNR 0848 023 WHILE WORKING NR 0748 DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, TENSION LOAD STRAP AT BS 873, WL 177, RBL 65 - LBL 65. REMOVED, FABRICATED AND REPLACED TENSION STRAP AT BS 870, WL 177 FROM RBL 65 TO LBL 65 ON FWD SIDE OF WHEEL WELL Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00615Bulkhead Doubler · corrodedNR 0851 024 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD RT RING DOUBLER, AT BS 873, RBL 58, WL 183. REMOVED, FABRICATED AND REPLACED RT RING DOUBLER AT BS 870, RBL 58, WL 183 IAW FED-EX DRAWING 69-14467.Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, BulkheadSDR 97FDEA00614Bulkhead Web · corrodedCORROSION (C57-174-01) ON BS 870 BULKHEAD WEB, RBL 70 - LBL 70, WL 178 TO 138. *S/D* BLENDED, REMOVED CORROSION ON BS 870 BULKHEAD WEB, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED BS 870 BULKHEAD WEB PER FED SRM 51-10-1.Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, BulkheadSDR 97FDEA00613Bulkhead Doubler · corrodedNR 0847 026 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, LEFT RING DOUBLER AT 873, LBL 58, WL 183. REMOVED, FABRICATED AND REPLACED LEFT RING DOUBLER AT BS 870, LBL 58, WL 183 IAW FED-EX DRAWING 69-14467.Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, BulkheadSDR 97FDEA00611Spar · corrodedCORROSION (C57-174-01) ON BS 870 REAR SPAR LOWER CHORD, LBL 40 TO 45, WL 138. *S/D* REMOVED CORROSION, BLENDED ON BS 870 REAR SPAR LOWER CHORD. FOUND CHORD TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED SPAR CHORD PER EA NR 7-5710-36144.Sep 1, 1997 · N144FE · Boeing 72721C · Wing SparSDR UPS97224319Actuator · leakedINSPECTION TYPE-N/A, LOSS OF HYDS, GEAR EXTENDED MANUALLY. FOUND LEAK AT NR 5 LE SLAT ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW MM 27-81-3 2, SERVICED HYDS, RAN ENGINES, CYCLED ALL FLT CONTROLS, CKD FOR LEAKS, OK FOR SERVICE.Aug 29, 1997 · N934UP · Boeing 72721C · Leading Edge Slat ActuatorSDR 97FDEA00608Floorbeam · corrodedCORROSION (C53-224-02) ON TOP CHORD OF FLOORBEAM BS 480, RBL 8, WL 208. *S/D* REMOVED CORROSION ON TOP CHORD OF FLOORBEAM AT BS 480, RBL 8, WL 208 AND REPAIRED PER FED-EX SRM 53-10-8, SRM 53-10-1.Aug 29, 1997 · N143FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00590Stringer · corrodedNR 0508 018 CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380-460.Aug 27, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00589Floorbeam · corrodedCORROSION (C53-111-01(3)) ON LOWER CHORD OF FLOORBEAM AT BS 1130, RBL 26 TO 39, WL 200. *S/D* REPAIRED FLOORBEAM LOWER CHORD IAW FEDEX EA NR 7-5310-36166A.Aug 27, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00583Door Frame · crackedNR 0763 042 CRACKED FWD DOORWAY FRAME IN THE FWD CARGO BAY AT THE NR 3 DOOR STOP (END OF CRACK IS MARKED) BS 520, RBL 52, WL 169. REPAIRED CRACK AT FWD DOORWAY FRAME IN FWD CARGO BAY AT THE NR 3 DOORSTOP BS 520, RBL 52, WL 169 PER FED-EX SRM 53-10-6.Aug 26, 1997 · N143FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00582Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 2 RT, BS 480 TO 540, BS 560 TO 580.Aug 26, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00581Floorbeam · corrodedNR 0229 017 CORROSION (C53-111-01-02) ON FLOORBEAM BS 600, WL 200, LBL 20 TO RBL 25. REPAIRED FLOORBEAM AT BS 600, WL 200, LBL 20 TO RBL 25 IAW FED-EX EA NR 7-5310-35035 REV A.Aug 26, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00579Floorbeam · corrodedCORROSION (C53-224-06) ON NOT CLIP AND DOUBLER UNDER AFT SIDE OF UPPER FLOORBEAM CHORD AT BS 740, RBL 49 AND ON PREVIOUS BLEND OUT UNDER FWD SIDE OF UPPER CHORD AT RBL 47. *S/D* REMOVED OUT OF LIMITS AREAS ON NUTCLIPS AND DOUBLER UNDER AFT SIDE OF UPPER FLOOAug 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00578Clip · crackedCRACKED STRINGER CLIP BS 970, STR 7 RT. *S/D* DRILLED OUT FASTENERS AND REMOVED CRACKED STRINGER CLIP. POSITIONED NEW STRINGER CLIP INTO PLACE AND BACKDRILL. INSTALLED FAYING SURFACES WET WITH SEALANT AND INSTALLED NEW STRINGER CLIP. ALL WORK DONE PER FEDAug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00577Clip · crackedFOUR EACH CRACKED STRINGER CLIPS AT BS 1010 AT STR 6L, 2R, 7R, 8R. *S/D* REPLACED FOUR EACH STRINGER CLIPS AT BS 1010, STR 6L, 2R, 7R AND 8R PER FED SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00576Clip · crackedTWELVE EACH CRACKED STRINGER CLIPS AT BS 990 AT STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 4R, 3R AND 2R. * S/D* REMOVED STRINGER CLIPS AND INSTALLED NEW CLIPS AT BS 990, STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 3R, AND 2R PER FED SRM 53-10-1.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00575Clip · crackedCRACKED STRINGER CLIP AT BS 970 STR 5 RT. *S/D* REMOVED AND REPLACED STR CLIP AT BS 970, S5R IAW FED SRM 51-10-1 AND SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00573Clip · crackedFOUR CRACKED STRINGER CLIPS AT BS 1010 AT STR 6L, 2R, 7R, 8R. *S/D* REMOVED CRACKED STR CLIPS BS 1010 AT STR 6R, 2R, 7R, 8R. INSTALLED NEW STR CLIPS AT BS 1010, STR 6R, 2R, 7R, 8R PER FED-EX SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00572Chord · corrodedCORROSION (C53-111-01-02) ON BL 0 CHORD BS 500 TO BS 686, WL 200. *S/D* REMOVED AND REPLACED THE BL 0 CHORD BS 450 TO BS 740, WL 200 PER FED-EX SRM 51-10-01, AND SRM 51-30-02 AND PER BOEING DRAWING SR 27-53-009.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00571Stringer · corrodedNR 0298 012 CORROSION (C53-224-02) ON STRINGER 2 RT, BS 420-480. REPAIRED STR 2 RT, BS 420-480 IAW FED-EX SRM 53-10-3 AND 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00570Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 8 LT, BS 360 TO 460. *S/D* REMOVED CORRODED STRINGER AND REPLACED STRINGER BS 360 TO BS 460, STR 8 LT IAW FED-EX SRM 53-10-3 FIG 3.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00568Clip · crackedSIX EACH CRACKED STRINGER CLIPS AT BS 1070 AT STR 8L, 3L, 2L, 8R, 6R, 3R. *S/D* REPLACED 6 EACH STRINGER CLIPS AT BS 1070 AT STR 8L, 3L, 2L, 8R, 6R AND 3R PER FED-EX SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00567Clip · crackedSEVEN EACH CRACKED STRINGER CLIPS BS 1050 AT STR 6L, 5L, 4L, 3L, 2L, 5R, 3R. *S/D* REPLACED 7 EACH STRINGER CLIPS, BS 1050, STR 6L, 5L, 4L, 3L, 2L, 5R AND 3R PER FED-EX SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00566Clip · crackedSIX CRACKED STRINGER CLIPS AT BS 1030 AT STRINGERS 2L, 3L, 4L, 5L, 6L, 3R. *S/D* REMOVED 6 STRINGER CLIPS BS 1030, STR 2L, 3L, 4L, 5L, 6L AND 3R. INSTALLED NEW STRINGER CLIPS AT BS 1030, STR 4L, 5L, 6L AND 3R, IAW FED-EX SRM 51-30-2. STR CLIPS AT BS 1030 SAug 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00565Strap · corrodedNR 0382 CORROSION UNDER SEAT TRACK AT BS 388, RBL 65, WL 208. REMOVED CORROSION UNDER SEAT TRACK FLANGE. CORROSION ON SEAT STRAP FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPLACED STRAP PER FED-EX SRM 51-10-1. CORROSION CLEAN-UP PER FED-EX SRM 51-1Aug 22, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00563Stringer · crackedSTRINGER 26 LT AT BS 470 FOUND TO BE CRACKED. *S/D* REPAIRED STR 26L AT BS 470 PER FED-EX SRM 53-10-3.Aug 21, 1997 · N143FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
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