Boeing 727-22

Service difficulty reports · 1,282

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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"

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SDR 95FDEA01543Stringer · crackedWHILE WORKING NR 0081, DISCOVERED CRACKED STR AT BS 440 PLUS 15 STR 23R. ACCESSED AND REPAIRED STR AT BS 440 PLUS 15 STR 23R PER FEDEX SRM 53-10-3. INSTALLED AND LEAK CHECKED OXYGEN CYLINDERS.Oct 16, 1995 · N188FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA01542Strap · crackedWHILE WORKING NR 0562, FOUND REINFORCING STRAP CRACKED BS 1110 RBL 32 WL 132. REPAIRED REINFORCING STRAP AT BS 1110 RBL 32 WL 153 IAW FEDEX SRM 51-40-4.Oct 16, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01541Keel Beam · corrodedWHILE WORKING NR 0079, DISCOVERED CORROSION ON RT KEEL BEAM BS 1126 TO 1129, STR 29R TO BE OUT OF LIMITS.Oct 16, 1995 · N188FE · Boeing 72722 · Fuselage Main, KeelSDR DHL95707002Radar Rt Unit · malfunctionedWEATHER RADAR SPIKES WHEN AIRCRAFT IS IN TURBULENCE OF LIGHT AND GREATER INTENSITY. DIVERTED TO SAT AND LANDED WITHOUT INCIDENT. FOUND LOOSE WIRES IN RADAR JUNCTION BOX TERMINAL 56. TIGHTENED LOOSE WIRES PER MM 20-11, REMOVED AND REPLACED RADAR RECEIVER TRAOct 14, 1995 · N707DH · Boeing 72722 · Weather Radar SystemSDR 95FDEA01533Stringer · corrodedCORROSION ON STR 26R STA 385 RT, E-BAY. REMOVED DAMAGED AREA OF STR 26R FROM BS 377 TO 393 AND REPAIRED PER FEDEX SRM 53-10-3. ALODINED AND PRIMED ALL EFFECTED AREAS.Oct 10, 1995 · N188FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA01512Keel Beam · crackedLT/KEEL BEAM IS CRACKED AND CORRODED FROM BS 1077 TO 1085. REPAIRED LT/KEEL BEAM THAT WAS CRACKED AND CORRODED FROM BS 1077 TO 1085 AS PER ENGINEERING EO 7-5310-7-2356 REV C PART 4. UPON FASTENER INSTALLATION FOUND STR 29L TO HAVE DRILL START OUT OF LIMITS. Oct 9, 1995 · N188FE · Boeing 72722 · Fuselage Main, KeelSDR 95FDEA01493Shear Tie · corrosionWHILE WORKING KEEL BEAM NR0389, FOUND CORROSION ON THE SHEAR TIE AT BS 1070 BETWEEN STR 29 AND STR 28L AFTER REMOVING SEAL FOR ACCESS OF AREA. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED SHEAR TIE, DOUBLER, AND FILLER, ALODINED, PRIMED Oct 4, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01474Frame · damage holeHOLE ON BS 1010 RT FRAME ON THE I/B SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION, FIG 8 SHAPED. REPAIRED HOLE IN BS 1010 RT FRAME ON I/B SIDE OF STR 27R PER FEDEX SRM 51-40-3 FIG 1.Oct 2, 1995 · N188FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01473Frame · damaged holeHOLE ON BS 990 RT FRAME ON THE I/B SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION, FIG 8 SHAPED. REPAIRED HOLE IN BS 990 RT FRAME ON I/B SIDE OF STR 27R PER FEDEX SRM 51-40-3 FIG 1.Oct 2, 1995 · N188FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01437Frame · crackedWHILE WORKING ON EO 7-5310-7-2354E1, A CRACK WAS FOUND ON FRAME AT TOOLING HOLE LOCATED AT BS 1050, LBL 22.5 ABOVE STR 27L. REPAIRED CRACK FOUND ON FRAME AT TOOLING HOLE LOCATED AT BS 1050, LBL 22.5 ABOVE STR 27L AS PER FEDEX SRM 51-40-3.Sep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01436Frame · crackedHOLE ON BS 970, RT FRAME ON THE INBOARD SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION (FIGURED AND SHAPED). CUT OUT DAMAGE ON UPPER FLANGE OF FRAME AT STR 27R, BS 970, RT AREA. CUT OUT WAS .50 INCH BY 1 INCH. FABRICATED REPAIR PART AND ISep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01435Floor Beam · corrosionCORROSION (72C235-02) AND BARE METAL ON TOP CHORD AND WEB OF THE BS 600 FLOOR BEAM RBL 2-55 AND LBL 2-48, WL 202-208. REMOVED CORROSION AT BS 600, RBL 2-55 AND LBL 2-43, WL 202-208, RBL 11 - 41 WERE FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL THICKNESS WAS Sep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01434Floor Beam · corrodedCORROSION ON FLOOR BEAM STA 328, WL 208, LBL 18 - 45. REMOVED CORROSION AND TREATED BS 328, WL 208, LBL 45. FOUND CORROSION AT BS 328, WL 208, LBL 18 OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR. ALL PER FEDEX SRM 53-10-8, 53-10-1, 53-10-2.Sep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01426Skin · dentedDENT IN SKIN AT NOSE ACCESS DOOR, BS 227 RBL 5. REPAIRED DENT PER FEDEX SRM 53-30-3, AT BS 227 RBL 5 FUSELAGE SKIN.Sep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA01425Frame · crackedHFEC INSP EXHIBITS CRACK EMANATING FROM HOLE ON BS 1090 FRAME, O/B SIDE UPPER OF STR 27L. REPAIRED CRACKED FRAME AT BS 1090, O/B SIDE UPPER OF STR 27L PER FEDEX SRM 51-40-3 FIG 1.Sep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01424Floor Beam · corrosionCORROSION (72C235-02), ON TOP CHORD AND WEB OF BS 720 FLOORBEAM, RBL 13 TO 22, 47.5 TO 55, WL 206 TO 208.Sep 26, 1995 · N188FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01423Skin · delaminatedTHE L/W I/B AFT FLAP HAS AREA OF DELAMINATION ON LOWER SURFACE, APPROX 70 INCHES FROM I/B END ON FRONT SPAR. REPAIRED L/W I/B AFT FLAP LOWER SURFACE IAW FEDEX SRM 51-40-6.Sep 25, 1995 · N188FE · Boeing 72722 · Trailing Edge FlapsSDR 95FDEA01422Nose Chord · corrosionCORROSION EMANATING FROM BULGING LEVELING COMPOUND ON LOWER RT NOSE CHORD, BS 294.5 PLUS 17 RBL 17 WL 145. REMOVED AND REPLACED RT NOSE CHORD, BS 284.5 PLUS 17 TO 351 RBL 17 WL 145 IAW BAC DRAWING NR 6515724.Sep 25, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01421Floor Support · corrodedCORRODED INTERCOSTAL STA 277 TO 295 RBL 13 WL 208. REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT, STA 277 TO 295 RBL 13 WL 208.Sep 25, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01420Floor Beam · corrodedCORROSION AROUND FLOOR PANEL FASTENER HOLES AT FLOORBEAM STA 344 WL 208 RBL 19 LBL 55. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-02. REMOVED AND REPLACED 344 BEAM UPPER CHORD FROM SKIN TO SKIN PER FEDEX DRAWING NR SR 8753-007.Sep 25, 1995 · N188FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01419Floor Panel · corrosionCORROSION AROUND FLOOR PANEL FASTENER HOLE AT STA 312 LBL 45 WL 208. REPAIRED PER FEDEX SRM 53-10-8 FIG 7.Sep 25, 1995 · N188FE · Boeing 72722 · Fuselage Floor PanelSDR 95FDEA01418Skin · gougedTHE NR 6 SLAT L/E HAS SMALL GOUGES APPROX 28 INCHES FROM O/B END. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED ON NR 6 SLAT L/E APPROX 28 INCHES FROM O/B END IAW FEDEX SRM 57-50-1, 57-50-3, DWG 65-17302.Sep 25, 1995 · N188FE · Boeing 72722 · Leading Edge DevicesSDR 95FDEA01417Skin · lightning strikeTHERE ARE 24 LIGHTNING STRIKES ON SKIN, BS 360 TO 480 STR 23 TO 26R. REMOVED DAMAGE AND REPAIRED PER FEDEX SRM 53-30-3.Sep 25, 1995 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA01401Floorbeam · corrodedCORROSION (72C235-02), AROUND FASTENER HOLE ON BS 660 FLOORBEAM RBL 19 WL 208. REMOVED DAMAGE AT BS 660 FLOORBEAM RBL 19 WL 208 AND INSTALLED REPAIR PER FEDEX SRM 53-10-08 FIG 8. REMOVED .046 MATERIAL FROM ORIGINAL .125 THICKNESS FLANGE, FOUND TO BE OUT OF Sep 21, 1995 · N188FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 95FDEA01384Frame · crackedHFEC INSP EXHIBITS CRACK EMITTING FROM HOLE ON BS 1070 FRAME ON THE O/B SIDE UPPER OF STR 27L. REPAIRED CRACK IN FRAME AT BS 1070 O/B SIDE OF STR 27L, WORK DONE IAW PER FEDEX SRM 51-40-3.Sep 18, 1995 · N188FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA01383Shear Tie · crackedFOUND CRACKED SHEAR TIE STA 312L BETWEEN STR 22 TO 23L, DOG HOUSE. REMOVED CRACKED SHEAR TIE AT BS 312 BETWEEN STR 22 TO 23L AND INSTALLED REPLACEMENT SHEAR TIE WET WITH SEALANT.Sep 18, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01382Clip · mis mfgTHERE IS NO RADIUS AT STR CLIP CUTOUT, BS 420 STR 5 TO 6R. REMOVED AND REPLACED STR CLIPS AT BS 420 STR 5 TO 6R.Sep 18, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01381Clip · mis mfgTHERE IS NO RADIUS AT STR CLIP CUTOUT, BS 400 STR 5R. REMOVED AND REPLACED STR CLIP AT BS 400 STR 5R.Sep 18, 1995 · N188FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01336Actuator · malfunctionedDURING CLIMBOUT FROM MEM WHEN RETRACTING FLAPS FROM 2 DEGREES TO ZERO, NR 7 SLAT RETRACT, RECYCLED FROM 2 TO ZERO 3 TIMES, BUT NR 7 SLAT REMAINED EXTENDED. REMOVED NR 7 SLAT ACTUATOR, CAPPED LINES. INSTALLED NR 7 SLAT ACT PER MM 27-81-32, OPS AND LEAK CK GOOSep 13, 1995 · N150FE · Boeing 72722 · Leading Edge Slat ActuatorSDR 95FDEA01335Retract Mech · malfunctionedDURING CLIMBOUT FROM MEM, WHEN RETRACTING FLAPS FROM 2 DEGREES TO ZERO, LED NR 7 WOULD NOT RETRACT. RECYCLED FLAPS FROM 2 DEGREES TO ZERO THREE TIMES, BUT LED NR 7 REMAINED EXTENDED EACH TIME. INSPECTED ACT INST AND SWS, ALL CK GOOD. SUSPECT AIR IN SYS, CYSep 13, 1995 · N150FE · Boeing 72722 · Leading Edge Slat Control SystemSDR 95FDEA01315Skin · corrodedSTR 9R STA 1352 TO 1420 PILLOWING SKIN. REMOVED AND REPLACED 30 INCHES OF SKIN AND REPAIRED SKINS BOTH FWD AND AFT OF STA 1365.5 STR 9R, PER FEDEX SRM 53-30-3, 51-30-2.Sep 12, 1995 · N147FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA01313Chord · corrodedCORROSION ON REINFORCEMENT CHORD STA 1176.9 RBL 55 WL 208. REMOVED PARTS, SECONDARY STRUCTURE AND REMOVED CORRODED REINFORCEMENT CHORD. INSTALLED NEW CHORD AND SECONDARY STRUCTURE. ALL WORK DONE IAW FEDEX SRM 53-10-1, 51-30-2. REPLACED CHORD BS 1176.9 LBL Sep 12, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01312Chord · corrodedCORROSION FOUND ON HORIZONTAL CHORD AT RBL 16.5 TO 20 WL 191.5. REPAIRED CORRODED AREA PER EA 7-5310-25687.Sep 12, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01292Chord · corrosionNR 0232 043. CORROSION C53-132-2(1) ON STA 870 LOWER CHORD LBL 70, 38-41, RBL 20, WL 156. REMOVED AND REPLACED BS 870 LOWER CHORD, LBL 70, WL 156 PER FEDEX EA 7-5710-29709.Sep 12, 1995 · N195FE · Boeing 72722 · Wing Miscellaneous StructureSDR 95FDEA01316Floor Support · corrodedFLOOR SUPPORT FLANGE AT STA 840 LBL 24 WL 208 HAS INTERGRANULAR CORROSION THAT IS OUT OF LIMITS. FABRICATED REINFORCEMENT STRAP PER EWO NO 95-3069.Sep 8, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01314Skin · corrodedSTRINGER 9L STA 1372 TO 1389 PILLOWING SKIN. REMOVED DAMAGE SECTION OF SKIN AND REPAIRED IAW FEDEX SRM 53-30-3, 51-30-2.Sep 8, 1995 · N147FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA01272Stiffener · gougedGOUGE IN FLOORBEAM VERTICAL STIFFENER STA 312 RBL 52 WL 207. REMOVED AND FABRICATED FLOORBEAM VERTICAL STIFFENER. ALL WORK DONE IAW FEDEX SRM 53-20-1.Sep 7, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA01271Seat Track · corrodedCORRODED SEAT TRACK AND FASTENERS AT STA 760 TO 850 LBL 25. REMOVED AND REPLACED SEAT TRACK. ALL WORK DONE IAW FEDEX SRM 53-10-1 AND FEDEX MM 53-20-12.Sep 7, 1995 · N147FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR KT3R643LT-Chord · corrodedSEVERE EXFOLIATING CORROSION FOUND ON SEC 41, LOWER RT T-CHORD AT BS 335 AND BS 350, RBL 18; CORROSION FOUND AFTER SKIN WAS OPENED UP TO INVESTIGATE CAUSE OF SKIN PILLOWING BETWEEN FASTENERS AND DISHED HEADS ON RIVETS. CORROSION LIMITED TO T-CHORD ONLY. INSPAug 23, 1995 · N32719 · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95ZZZX4288Sense Line · brokenDURING CRUISE, NR 3 ENGINE'S FUEL FLOW AND EGT BEGAN TO CLIMB WITH LOWER RPM'S AT SAME THROTTLE SETTING AS NR 1 AND NR 2 ENGINES. OK, PRESSURE GOOD, NO VIBRATION NOTED. REDUCED POWER TO IDLE FOR ABOUT 1.50 HOURS, INBOUND TO EWR. FOUND 13TH STAGE AIR PRESSURAug 1, 1995 · N400RG · Boeing 72722 · Compressor Bleed ControlSDR 95FDEA00849Post · crackedRIGHT NR 2 WINDOW CUT OUT DOUBLER IS CRACKED IN THE UPPER AFT RADIUS. REPAIRED CRACK IN DOUBLER IAW EO 7-5330-7-3354 PART 5.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00848Spar · corrodedCORROSION FOUND ON UPPER REAR SPAR CHORD BS 870 AT RBL 20 AND LBL 10. REMOVED AND REPLACED UPPER REAR SPAR CHORD AT BS 870 PER EA NR 95-2684 AND DWG NR 65C21531-2.Jun 28, 1995 · N180FE · Boeing 72722 · Wing SparSDR 95FDEA00847Keel Beam · corrodedRIGHT KEEL BEAM CORRODED, BS 953, RBL 6, WL 156. CUT ACCESS HOLE IN SKIN, REMOVED AND REPLACED KEEL BEAM THEN REPAIRED HOLE IN SKIN. REF: TCO EWO NR 95-2710 AND SRM 53-30-3 FIG 3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, KeelSDR 95FDEA00846Frame · crackedAFT CARGO BAY BS 1130 STR 27L, FRAME IS CRACKED. CUT OUT DAMAGE AND REPAIR PER SRM 51-40-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00845Fitting · corrodedSTA 351, CORROSION ON STR 26R DOG BONE FITTING. REMOVED AND REPLACED STR 26R STA 351. FITTING IAW FEDEX SRM 51-30-2.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00844Frame · damagedFOUND FIGURE EIGHT HOLE IN FRAME FLANGE AT STA 1030 STR 27R. TRIMMED OUT DAMAGED PORTION OF FRAME, FABRICATED REPAIR PART AND INSTALLED WET WITH SEAL AS PER SRM 51-40-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00843Frame · crackedCRACKED FRAME AT BS 1070 STR 27L. REMOVED AND REPLACED FRAME AT BS 1070 STR 24-27L AND TREATED IAW FEDEX SRM 51-40-03, FEDEX MM 51-20-31 AND 51-20-21.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00842Frame · crackedCRACKED FRAME AT BS 1090 STR 27L. REMOVED AND REPLACED FRAME BS 1090 STR 24-27L AND TREATED IAW FEDEX SRM 57-40-03, FEDEX MM 51-20-31 AND 51-20-21.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00841Stringer · crackedSTR 23L IS CRACKED AT STA 380. REMOVED AND REPLACED STR 23L STA 360-384 IAW FEDEX SRM 53-10-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00840Stringer · crackedPOSSIBLE CRACKS ON STR 24L BS 380. REMOVED DAMAGED STR, FABRICATED REPAIR PARTS AND INSTALLED IAW FEDEX SRM 53-10-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
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