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.

SDR 96FDEA00534Spar Chord · corrosionCORROSION (C53-132-02, 1) ON THE WING CENTER LOWER SPAR CHORD STA 870 LBL 36 TO 40 WL 138. REMOVED AND REPLACED LOWER SPAR CHORD.Mar 11, 1996 · N187FE · Boeing 72722 · Wing SparSDR 96FDEA00510Chord · corrosionNR 400, CORROSION (C53-111-03) ON RT MID NOSE CHORD VERTICAL FLANGE EMANATING FROM BENEATH A VERTICAL STIFFENER BS 518 AND TWO BULGES IN FLOOR WEB ON CHORDS HORIZONTAL FLANGE BS 318 AND 335, RBL 15, WL 159, ACCESS REQUIRED. *S/D* REMOVED AND REPLACED RT MID Mar 11, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00507Sill Strap · corrosionNR 0217, CORROSION (C53-113-01, 2) ON SILL STRAP AT BS 1057 RBL 20 WL 149. REMOVED AND REPLACED SILL STRAP BS 1120 TO 1030 RBL 20 WL 149.Mar 11, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00506Stringer · corrosionNR 0078 (C53-113-01) ON THRESHOLD VERTICAL WEB UNDER NUTPLATES BS 540 AND 560, RBL 21, WL 156. *S/D* REMOVED DAMAGED PORTION OF STRINGER AT BS 480, STR 27R, WL 157. REPAIRED STRINGER IAW FEDEX SRM 53-10-3.Mar 11, 1996 · N187FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00505Threshold Web · corrosionNR 0078, (C53-113-01) ON THRESHOLD VERTICAL WEB UNDER NUTPLATES BS 540 AND 560, RBL 21, WL 156. *S/D* REMOVED AND REINSTALLED VERTICAL WEB IAW SRM 53-10-1.Mar 11, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00504Skin · dentedNR 0071, BS 660-3 STR 20R, WL 181, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE, OUT OF LIMITS PER SRM 53-30-1. *S/D* REMOVED GOUGE IN SKIN AT BS 660.3 STR 20R, WL 181, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3.Mar 11, 1996 · N187FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00551Fitting · corrodedCORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING ON VERTICAL STABILIZER AT BS 1342 LBL 17 AT STR 5L PER SB 727-55-00.Mar 10, 1996 · N194FE · Boeing 72722 · Vertical StabilizerSDR 96FDEA00512Skin · delaminationNR 412, LT WING I/B AFT FLAP HAS TWO AREAS OF DELAMINATION ON UPPER SURFACE T/E 36 INCHES FROM END. ACTUAL DAMAGE IS ON LOWER SURFACE APPROX 12.5 BY 5 INCHES. REPAIRED DELAMINATION ON UPPER SURFACE SRM 51-40-6.Mar 8, 1996 · N187FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00511Skin · delaminationNR 407, RT WING O/B AFT FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE 72 INCHES FROM O/B END. ACTUAL DAMAGE IS 38.25 BY 3.5 INCHES. REPAIRED DAMAGE ON UPPER SURFACE SRM 51-40-06.Mar 8, 1996 · N187FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00487Track · crackedSNRM (0384), RT WING OB MIDFLAP HAS A 2 INCH CRACK ON LOWER SURFACE T/E JUST BELOW I/B OF OB AFT FLAP TRACK ASSY. REMOVED, FABRICATED AND INSTALLED NEW U-CHANNEL AND INSTALLED NEW TRACK ASSEMBLY MM 27-51-56.Mar 8, 1996 · N187FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00486Rib · gougedSNRM (0109), FIXED LEADING EDGE LEFT WING HAS GOUGES JUST O/B OF NR 1 SLAT ON VERTICAL RIB. REMOVED AND REPLACED VERTICAL RIB.Mar 8, 1996 · N187FE · Boeing 72722 · Wing, Rib/BulkheadSDR 96FDEA00485Threshold Plate · corrodedSNRM 0087, CORROSION (C53-224-04) AFT ENTRY DOOR THRESHOLD SUPPORT PLATE BS 1176, WL 209 LBL 11 TO RBL11. *S/D* REPLACED THRESHOLD SUPPORT PLATE.Mar 8, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00418Bear Strap · corrosionCORROSION (C53-113-01, 2) ON BEAR STRAP AT BS 1080 RBL 24 WL 145. REMOVED AND REPLACED LOWER PORTION OF BEAR STRAP PER EA 7-5310-28793.Mar 7, 1996 · N187FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00417Skin · gougeBS 277.2 STR 21R WL 180, THERE IS A DEEP GOUGE IN SKIN. *S/D* BLENDED GOUGE IN SKIN AT BS 277.2 STR, WL 180. ORIGINAL SKIN THICKNESS WAS 040, AREA REMOVED WAS 030 IN A 1 BY 5 INCH AREA AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. DAMAGED AREA WAS REPAMar 7, 1996 · N187FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR CA960315002Flange · cracked(CAN)AFTER TAKEOFF THE AFT BODY OVERHEAT LIGHT CAME ON. FUEL DUMPED AND RETURNED TO BLOCKS. CRACK IN FLANGE OF PURGE VALVE. REPLACED.Mar 6, 1996 · Boeing 72722 · Heating SystemSDR 96FDEA00407Mid Spar · wornVERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 RT. REPAIRED PER FEDEX EA 7-5510-27728.Mar 5, 1996 · N194FE · Boeing 72722 · Vertical Stabilizer, Spar/RibSDR 96FDEA00373Fitting · corrodedCORROSION 26L BS 360 FITTING. REPLACED STR TIE FITTING AT STR 26L, BS 360 AND MADE STR REPAIR ON STR 26L FROM BS 360 TO 390. DAMAGE ON THAT PORTION OF STR WAS FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1 FEDEX SRM 53-10-3.Mar 4, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00383Doubler · crackedWHILE WORKING CARD NR 71C102-01, FOUND RADOME TO BE MISALIGNED AT BS 178, ALLOWING RADOME TO CATCH DOUBLER WHICH CRACKED DOUBLER AND CHIPPED RADOME WL 235 LBL 4. *S/D* REPLACED RADOME WL 235, LBL 4 PER FEDEX SRM 53-50-4 AND REPAIRED SKIN DOUBLER BS 178, WL 2Mar 1, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00381Blkhd Support · corrodedREMOVED VERTICAL CHORD TO ACCESS TERMINAL FITTING AND DISCOVERED CORROSION ON BULKHEAD SUPPORT CHANNEL, BS 1342 WL 238 TO 246 RBL 24. REMOVED AND REPLACED BS 1342 BULKHEAD SUPPORT CHANNEL OF BS 1342 RBL 24 WL 193 TO 258.Mar 1, 1996 · N194FE · Boeing 72722 · Fuselage Main, BulkheadSDR 96FDEA00371Stiffener · crackedWHILE WORKING 7-5310-7-3367B PT 1, DISCOVERED A CRACK IN THE FWD PRESSURE PAN STIFFENER AT BS 740 WL 208 LT. ALSO, FOUND FWD PRESSURE PAN DAMAGED, FABRICATED NEW STIFFENER AND RIVETED TOGETHER NEW PAN. ALL WORK ACCOMPLISHED PER FEDEX SRM 51-20-1 AND BOEING DMar 1, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00370Stringer · damagedMECH DAMAGE ON STR 25L BS 560 WL 154. REPAIRED DAMAGED STR AT BS 560 STR 25L WL 154 PER FEDEX EA 7-5310-27491.Mar 1, 1996 · N194FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00367Web · crackedCRACK IN WEB AT BS 520 WL 198 RBL 58. REMOVED, FABRICATED NEW WEB AND INSTALLED THE WEB AT BS 500 TO 560 RBL 58 WL 198, AS PER BOEING DRAWING 65-19309.Mar 1, 1996 · N104FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00366Chord · corrosionAREA OF CORROSION ON BS 1342 CHORD UPPER FWD RT FLANGE RBL 20. REMOVED AND REPLACED UPPER CHORD IAW FEDEX DRAWING 65-17508.Mar 1, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00380Floor Beam · double drilledWHILE WORKING NR0308 FOUND HOLE IN RADIUS OF FLOOR BEAM LOWER CHORD BS 580 BL 0 WL 200. *S/D* REPAIRED FLOOR BEAM PER SRM 53-10-8.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00379Intercostal · dentedDENTED INTERCOSTAL BS 1055 BETWEEN STR 23 TO 25L LBL 36 TO 48 WL 156. *S/D* REMOVED AND REPLACED OUT OF LIMITS INTERCOSTEL PER FEDEX SRM 53-10-1.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00378Mid Spar · wornVERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LT. REPAIRED PER FEDEX EA 7-5510-27728.Feb 28, 1996 · N194FE · Boeing 72722 · Vertical Stabilizer, Spar/RibSDR 96FDEA00377Vert Mid Spar · wornVERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LEFTSIDE. *S/D* REPAIRED PER FEDEX EA 75510-27728.Feb 28, 1996 · N194FE · Boeing 72722 · Elevator, Spar/RibSDR 96FDEA00376Spar Chord · corrosionCORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. *S/D* REMOVED AND REPLACED UPPER CHORD PER FEDEX EA 7-5710-27481.Feb 28, 1996 · N194FE · Boeing 72722 · Wing SparSDR 96FDEA00372Threshold Web · corrodedCORROSION (C53-111-01-1) ON DOOR THRESHOLD VERTICAL WEB, BS 527 RBL 22 WL 156. REMOVED, FABRICATED AND INSTALLED VERTICAL AND HORIZONTAL WEB PER SRM 53-10-1.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00369Fail-Safe · corrodedCORROSION (53-111-01-1) ON THE FAIL-SAFE AT BS 380 STR 26L WL 150 AROUND I/B FASTENER HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00368Strap · corrodedCORROSION (C53-111-01-2), ON FWD CARGO BAY THRESHOLD STRAP, BS 520 RBL 24 WL 156. REMOVED AND REPLACED THE FWD CARGO BAY THRESHOLD STRAP BS 500 TO 580 RBL 24 WL 156.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00360Chord · corrodedCORROSION (C53-224-08), ON BS 1176 CHORD AT LBL 20 AND RBL 65 WL 208. REMOVED AND REPLACED 1176 CHORD PER 51-30-2.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00358Floor Beam · corrodedCORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 600 LBL 20 TO RBL 26 WL 200. REMOVED CORRODED AREA FROM LBL 17 TO RT SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-8 FIG 2.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00357Shear Web · corrodedCORROSION (C53-224-02), ON SHEAR WEB AT BS 1173 RBL 27 WL 208. REPAIRED SHEAR WEB PER SRM 51-40-2.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00356Skin · gougedTHREE GOUGES IN SKIN AT BS 590 TO 620, BETWEEN STR 21 TO 22R. REPAIRED 3 GOUGES IN THE SKIN AT BS 590 TO 620, BETWEEN STR 21 TO 22R PER FEDEX SRM 53-30-3.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00355Shear Tie · crackedSHEAR TIE IS CRACKED AT FASTENER HOLE, BS 1166 BETWEEN STR 25 TO 26R. REPAIRED CRACKED SHEAR TIE PER FEDEX SRM 53-10-4 FIG 14.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00354Skin · corrodedBULGING AROUND FASTENERS ON EXTERIOR SKIN BS 227.8 RBL TO LBL 5. REPAIRED BULGING SKIN AT BS 227.8 RBL TO LBL 5 AS PER FEDEX SRM 53-30-3.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00353Skin · corrodedWHILE WORKING NR0007, FOUND CORROSION IN UPPER SKIN LAP BS 1142 TO 1148 STR 26R. REPAIRED SKIN PER SRM 53-30-3 AND SB 727-53-0072.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00351Blkhd Web · corrosionON REMOVAL OF THE REAR, UPPER AND LOWER SPAR CHORDS, FOUND 870 BULKHEAD WEB HAS CORROSION, LBL TO RBL 70 WL 174 TO 140. REMOVED AND REPLACED 870 BULKHEAD WEB.Feb 28, 1996 · N194FE · Boeing 72722 · Fuselage Main, BulkheadSDR 96FDEA00331Trim Motor · failedAFTER TAKEOFF, MAIN STABILIZER TRIM FAILED. RESET CIRCUIT BREAKER TO NO AVAIL, CRUISE TRIM WORKED NORMALLY. REPLACED MAIN ELECTRIC STABILIZER TRIM MOTOR PER MM 27-40-31 PAGE 201, OPS CHECK GOOD.Feb 28, 1996 · N147FE · Boeing 72722 · Stabilizer Control SystemSDR 96FDEA00348Stringer · damageMECHANICAL DAMAGE ON STR 25L BS 560, WL 154. *S/D* REPAIRED DAMAGE STRINGER AT BS 560, STR 25L WL 154 PER FEDEX EA 7-5310-27491.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00342Floorbeam · corrodedCORROSION (C53-111-01, -3), ON LOWER CHORD OF 1110 FLOORBEAM WL 200 LBL 2 TO 30 AT NUTPLATE HOLES. REMOVED AND REPLACED CORRODED LOWER CHORD OF BS 1110 FLOORBEAM AT WL 200 RBL 4 TO LBL 19.75 WITH FABRICATED REPAIR PARTS PER SRM 53-10-8 FIG 2.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00341Blkhd Web · cutWHILE WORKING NR0788, FOUND A CUT IN 950 BULKHEAD VERTICAL WEB BL 0 WL 208 AFT SIDE. REPAIRED CUT IN 950 BULKHEAD VERTICAL WEB AT BL 0 WL 208 AFT SIDE PER FEDEX SRM 53-10-9 FIG 2.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, BulkheadSDR 96FDEA00340Stringer · corrosionCORROSION (C53-224-01, -2), ON STR 9R BS 930 PLUS 7 RT AREA IS OUT OF LIMITS. REPAIRED STR 9R IAW FEDEX SRM 53-10-3.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00339Web · corrosionCORROSION ON WEB AT BS 294.5 TO 355 RBL 10 TO 35 WL 169. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WEB PER SRM 51-40-02.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00338Skin · gougedGOUGE IN EXTERIOR SKIN BS 945 STR 9R. REMOVED DAMAGED SKIN, BS 945 STR 9R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 53-30-3.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00337Floorbeam · double drilledDOUBLE HOLE IN FLOORBEAM BS 500 BL 0 WL 208.1. REPAIRED DOUBLER HOLE AT BS 500 BL 0 WL 208 IAW FEDEX SRM 53-10-8.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00336Web · corrodedCORROSION (C53-111-01-1), ON DOGHOUSE WEB STA 303 TO 309 LT LBL 15 WL 177. REMOVED CORROSION FOUND MATERIAL LOSS WAS WITHIN LIMITS PER SRM 53-10-1. TREATED AREA, PRIMED AND REINSTALLED FASTENERS.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00335Skin · corrosioinBS 1110 STR 26, THERE IS BULGE IN SKIN TRIPLER DAMAGED OUT OF LIMITS. REPLACED BONDED DOUBLER AT BS 1148 TO 1166 STR 25 TO 26R. REPLACED BONDED TRIPLER FROM BS 1108 TO 1130 STR 25 TO 26R. REPAIRED REMAINING DEBONDED SKIN USING FIXED PATTERN PER FEDEX SRM 5Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00334Floorbeam · double drilledWHILE WORKING CARD NR0683, FOUND BS 600 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED FLOORBEAM BS 600 BL 0 WL 208 IAW FEDEX SRM 53-10-8.Feb 26, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor Beam
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