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 96FDEA00270Shear Tie · corrosionCORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 LBL 17 TO 22, FOUND WHILE WORKING NR0053 WL 146. REMOVED SHEAR TIE, REMOVED CORROSION, TREATED AND REINSTALLED IAW FEDEX SRM 53-10-1, 53-10-4.Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00269Frame · corrosionCORROSION FOUND ON DOOR FRAME BS 1057.5 WL 162 RBL 25, WHILE WORKING NR0053. REMOVED AND REPLACED FRAME IAW DRAWING 65-20728.Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00268Skin · corrosionEXTERIOR SKIN BULGE AND RIVET HEAD DISHED AT BS 1108, 4.5 INCHES UP FROM BOTTOM OF SKIN LAP STR 26R, AT AFT CARGO DOOR CUTOUT LOWER AFT CORNER. REPAIRED DAMAGED SKIN AT BS 1108 STR 26 RT SKIN LAP PER FEDEX EA 7-5330-27406.Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00267Hinge · corrodedFIXED L/E FITTING PER NR 1 K-FLAP CENTER LUG IS CORRODED. REPAIRED CENTER HINGE FITTING WITH NEW.Feb 16, 1996 · N193FE · Boeing 72722 · Leading Edge DevicesSDR 96FDEA00266Clip · corrodedCORROSION (C53-111-01-1), STRINGER CLIP STR 24L BS 380. REMOVED AND REPLACED STR CLIP AT STR 24L BS 380.Feb 16, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00265Skin · gougeGOUGE IN SKIN AT STA 688 RBL 30 BETWEEN STR 24 AND 25R. REPAIRED GOUGE IN SKIN AT STA 688 RBL 30 BETWEEN STR 24 AND 25R IAW FEDEX SRM 53-30-3, 53-30-1.Feb 16, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00264Skin · delaminatedLT WING O/B AFT FLAP HAS A 6 INCH BY 3 INCH DELAMINATED DENT ON LOWER SURFACE 30 INCHES FROM I/B END. REPAIRED DELAMINATION PER SRM 51-40-6.Feb 16, 1996 · N194FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00263Te Wedge · delaminatedLT WING O/B AILERON T/E WEDGE HAS AN AREA OF DELAMINATION ON I/B LOWER SURFACE 6 INCHES BY 4 INCHES. REPAIRED LT WING O/B AILERON T/E WEDGE PER FEDEX SRM 51-80-04 SRM 51-40-06.Feb 16, 1996 · N194FE · Boeing 72722 · AileronsSDR 96FDEA00262Frame · dentedDENT IN FRAME BS 1090 BETWEEN STR 23 TO 24L LBL 47 WL 169. REMOVED DAMAGE, FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 51-40-3.Feb 16, 1996 · N194FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00260Stringer Clip · crackedDAMAGED STR CLIP BS 420 STR NR 4 LT. REMOVED AND REPLACED DAMAGED STR CLIP AT BS 420 STR 4 LT.Feb 16, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00258Frame Splice · damagedFRAME SPLICE DAMAGE AT BS 1010 RT WL 157 RBL 41 BETWEEN STR 24 TO 25R. REMOVED DAMAGED FRAME SPLICE AT BS 1010 RT WL 157 RBL 14. FABRICATED NEW FRAME SPLICE AND INSTALLED.Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00257Frame · crackedCRACK AND MULTIPLE STOP DRILLS ON UNDERSIDE OF FRAME AT BS 930 BETWEEN STR 15 TO 14R. REPAIRED CRACK AND MULTIPLE STOP DRILLS ON UNDERSIDE OF FRAME AT BS 930, BETWEEN STR 15 TO 14R IAW FEDEX EA 7-5310-27450.Feb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00256Keel Beam · corrosionEXTERIOR SKIN, BULGE IN SKIN AT KEEL BEAM STR 29L BS 1050 TO 1030. REMOVED CORROSION ON KEEL BEAM BS 1030 TO 1050 STR 29L, FOUND TO BE OUT LIMITS PER FEDEX SRM 53-10-1. REMOVED FRAMES BS 970, 990, 1010, 1050, 1070 AND 1030. REMOVED KEEL BEAM, INSTALLED NEWFeb 16, 1996 · N193FE · Boeing 72722 · Fuselage Main, KeelSDR 96FDEA00249Shear Web · corrodedWHILE WORKING CARD NR 0583, FOUND BS 540 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED FLOOR BEAM AT BS 540, BL 0, WL 208 IAW FEDEX SRM 53-10-8.Feb 16, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00230Floor Beam · corrodedCORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOOR BEAM AT BS 640 LBL 23 TO RBL 26.7 WL 200. *(S/D)* REMOVED AND CORRODED ON LOWER FLANGE OF FLOOR BEAM IN NUTPLATE HOLES AT BS 640 LBL 23 TO RBL 26.7 WL 200. REPAIR PARTS PER FDE SRM 53-10-8.Feb 16, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00253Floorbeam · misdrilledWHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 990 FLOORBEAM AT BL 0 WL 208.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00252Floorbeam · misdrilledWHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 970 FLOORBEAM AT BL 0 WL 208.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00251Floor Beam · double drilledWHILE WORKING CARD NR 0683, FOUND BS 600 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED FLOOR BEAM BS 600, BL 0, WL 208 IAW FEDEX SRM 53-10-8, HOLE PER SRM 53-10-8.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00250Floor Beam · double holeWHILE WORKING CARD NR 0685, FOUND BS 580 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED DOUBLE HOLE PER SRM 53-10-8 SRM 53-10-8.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00248Shear Web · corrodedCORROSION EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 5, LBL 20 WL 208. *S/D* FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00247Stringer · gougedWHILE WORKING NR0429, FOUND GOUGE ON STR NR 3 BS 640 RT.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00246Web · mech damageMECHANICAL DAMAGE AND MISDRILLED HOLES IN WEB AT BS 560 TO 580 LBL 41 WL 200.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00245Frame · crackedTHE FRAME AT BS 580 IS CRACKED ON I/B FLANGE AT RBL 67, WL 210. *S/D* THE FRAME AT BS 580, RBL 67, WL 210, WAS FOUND TO BE DAMAGED BEYOND LIMITS PER SRM 53-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00244Stringer · gougeGOUGE IN STR BS 400 STR 16R. REPAIRED GOUGE IN STR BS 400 STR 16R PER FEDEX SRM 53-10-03 FIG 2.Feb 14, 1996 · N194FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00240Floorbeam · corrodedCORROSION (C53-224-01) ON UPPER CHORD OF BS 950 FLOORBEAM AT RBL 21 WL 208. CLEANED AND TREATED CORROSION ON UPPER CHORD OF BS 950 FLOORBEAM AT RBL 21 WL 208, FOUND TO BE WITHIN LIMITS PER FEDEX EA 7-5310-27447.Feb 14, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00239Shear Tie · corrosionCORROSION ON BOTTOM OF SHEAR TIE BS 970 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR0053. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE IAW FEDEX SRM 53-10-4, CLEANED UP AREA AND INSTALLED SHEAR TIE.Feb 14, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00261Frame · dentedDENT IN FRAME AT BS 1010 LBL 39 WL 153. FABRICATED PART AND REPAIRED FROM PER SRM 51-40-03.Feb 13, 1996 · N194FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00259Tie Wedge · delaminatedRT WING I/B MIDFLAP TIE WEDGE HAS AN AREA OF DELAMINATION ON O/B END 12 INCHES BY 3 INCHES. REPAIRED DELAMINATION PER SRM 51-40-6.Feb 13, 1996 · N194FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00236Shear Tie · damagedOBLONGED HOLE ON SHEAR TIE AT BS 1030 RBL 42 WL 165, FOUND WHILE WORKING NR 0053. CUT OFF DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1030 RBL 42 WL 165 PER FEDEX SRM 53-10-4.Feb 12, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00235Shear Tie · corrosionCORROSION (C53-111-01,-3) AFT CARGO BAY, ON SHEAR TIE AT BS 1030 RBL 4 WL 138.5. REPAIRED SHEAR TIE AT BS 1030 RBL 4 WL 138.5 AS PER FEDEX SRM 53-10-4.Feb 12, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00234Floorbeam · corrodedCORROSION (C53-224-06) ON FLOORBEAM AT BS 620 RBL 10 TO 43 WL 208. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED REPAIR PARTS, CLEANED, TREATED AND INSTALLED PARTS. ALL WORK ACCOMPLISHED IAW FEDEX SRM 53-10-8 AT BS 620 RBL 10 TO 43 WL 208.Feb 12, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00228Frame · dentedDENT IN FRAME BS 1050 BETWEEN STR 25 TO 26L LBL 30 WL 153. REPAIRED DENT IN FRAME AT BS 1050 BETWEEN STR 25 TO 26L LBL 30 WL 153 PER FEDEX SRM 51-40-3 FIG 1.Feb 12, 1996 · N194FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00226Channel · corrosionCORROSION (C-53-111-01, -3) ON NR 2 CARGO DOORWAY C-CHANNEL BS 1057 TO 1110 RBL 27, WL 147. *S/D* REMOVED AND REPLACED C-CHANNEL AT DOORWAY.Feb 12, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00284Skin · corrosionCORROSION (C53-100-01-4), BS 1080 TO 1110 STR 26 LT AND RT. ALSO, DEEP GOUGES ON EXTERIOR SKIN. MECHANICALLY REMOVED CORROSION FROM EXTERIOR SKIN, BS 1080 TO 1110 STR 26 LT AND RT. FOUND A 1.5 INCH BY 1.5 INCH AREA AT STR 27L BS 1090 TO BE OUT OF LIMITS PERFeb 9, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00271Shear Tie · corrosionCORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 17 TO 22 WL 146, FOUND WHILE WORKING NR0053. REMOVED SHEAR TIE, REMOVED CORROSION, TREATED AND REINSTALLED SHEAR TIE FEDEX SRM 53-10-1.Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00233Bonding Strap · corrosionCORROSION (097-562-01-2) NR 4 RT FLAP BULLNOSE OB BONDING JUMPER UPPER ATTACH POINT AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME. *S/D* REMOVED CORROSION PER FEDEX SRM 57-50-3 AND 27-57-010.Feb 9, 1996 · N194FE · Boeing 72722 · Leading Edge DevicesSDR 96FDEA00232Skin · delaminationLEFT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON I/B UPPER AND LOWER SKIN 18 INCHES BY 18 INCHES. REPAIRED DELAMINATION PER SRM 51-40-06.Feb 9, 1996 · N194FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00231Tie Wedge · delaminatedRT WING I/B MIDFLAP TIE WEDGE HAS AN AREA OF DELAMINATION ON O/B END 12 INCHES BY 3 INCHES.Feb 9, 1996 · N194FE · Boeing 72722 · Trailing Edge FlapsSDR 96FDEA00229Floorbeam · corrodedCORROSION AT BS 540 FLOORBEAM LOWER CHORD FROM LBL 16 TO RBL 28 WL 200.Feb 9, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00227Floor Beam · corrodedCORROSION (C53-111-01, -3) ON LOWER CHORD OF 1110 FLOOR BEAM WL 200 LBL 2 TO 30 AT NUTPLATE HOLES. *S/D* REMOVED AND REPLACED CORRODED LOWER CHORD AT BS 1110 FLOOR BEAM AT WL 200, RBL TO LBL 19.75 WITH FABRICATED REPAIR PARTS PER SRM 53-10-8 FIG 2 PER FEDEX Feb 9, 1996 · N194FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00225Skin · creaseBS 1120 BETWEEN STR 17 TO 19L, THERE IS A CREASE IN SKIN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-30-3.Feb 9, 1996 · N194FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA00224Shear Tie · corrosionCORROSION ON BOTTOM OF SHEAR TIE BS 1030 LBL 3 TO 4 WL 146, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REPAIR AT BS 1030 LBL 3 TO 4 WL 146 IAW FEDEX SRM 53-10-4 FIG 15.Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00223Frame · crackedBS 1070 FRAME CRACK EMITTING FROM STOP DRILL HOLE AT BL 0 TO BL 10 WL 150, FOUND WHILE WORKING CUSTOMER CARD NR 0053. REMOVED DAMAGE FROM FRAME BS 1070 AT BL 0 AND LBL 10 WL 150, FABRICATED FILLERS AND INSTALLED IAW SRM 51-40-3 AND PREVIOUS REPAIR DOUBLER REIFeb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA00221Hinge · corrodedCORROSION ON RT WING O/B AILERON NR 3 HINGE. REMOVED CORRODED NR 3 HINGE, INSTALLED A NEW HINGE AND REINSTALLED RT WING O/B AILERON IAW FEDEX MM 27-10-31, FUNCTIONAL TESTED IAW FEDEX MM 27-10-00.Feb 9, 1996 · N193FE · Boeing 72722 · AileronsSDR 96FDEA00220Floorbeam · corrodedCORROSION ON FLOORBEAM (C53-224-01(1), BS 344 WL 208 RBL 15 TO 50 AROUND NUT CLIP HOLES UPPER AND LOWER SURFACE. REMOVED UPPER CHORD OF FLOORBEAM BS 344 FABRICATED AND INSTALLED NEW UPPER CHORD OF FLOORBEAM PER FEDEX SR 27-53-007.Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00219Stringer · damagedINTERCOSTAL BETWEEN BS 1130 AND 1149 HAS FASTENER PULLED THROUGH STR 6R. CUT OUT STR DAMAGE AREA FABRICATED STR SPLICES REPAIR AND INSTALLED REPAIR PARTS WITH FASTENERS PER FEDEX SRM 53-10-3 FIG 3 AT BS 1130 AND 1149 STR 6R.Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA00218Keel Beam · corrosioinEXTERIOR SKIN BULGE IN SKIN AT KEEL BEAM STR 29L BS 1050 TO 1030.Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, KeelSDR 96FDEA00217Floorbeam · corrodedCORROSION (C53-224-06), ON FLOORBEAM OF BS 600 RBL 10 TO 30 WL 208. REMOVED CORRODED SECTION OF FLOORBEAM FABRICATED REPAIR ANGLES AND INSTALLED ALL WORK DONE PER FEDEX SRM 53-10-8.Feb 9, 1996 · N193FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA00216Shear Tie · damagedMECHANISM DAMAGE ON SHEAR TIE AT BS 600 BETWEEN STR 16 TO 17R.Feb 9, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA00215Shear Tie · corrodedCORROSION (C53-111-01,3) ON SHEAR TIE AT BS 970 RBL 10.Feb 9, 1996 · N194FE · Boeing 72722 · Fuselage Miscellaneous Structure
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