Boeing 727-25

Service difficulty reports · 827

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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 = '72725'
  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 96FDEA00697Stringer · damageNR0604 AND 036, WHILE WORKING NR0156, FOUND MECH DAMAGE ON STR 24 AT STA 482.Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00696Skin · corrodedCORROSION C53-113-01(2). FOUND WHILE WORKING NR 0240 FWD AND AFT CORNERS OF DOOR THRESHOLD STA (1107) TO 1060, WL 160, RBL 37. *****S/D**** REPLACED BARE STRAP LOWER HALF IAW EA 7-5310-28087.Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00693Floor Beam · corrodedCORROSION (C53-224-01) ON FLOOR BEAM BS 360 LBL 12 RBL 5 AND 48 WL 208. REPAIRED FLOOR BEAM BS 360 LBL 12 AND RBL 5 WL 208. FOUND FLOOR BEAM BS 360 RBL 48 TO BE WITHIN SERVICEABLE LIMITS. CLEANED AND TREATED BS 360 RBL 48 WL 208 PER FEDEX SRM 51-10-6. REPAMar 25, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00692Stringer Clip · gougedMECH DAMAGE TO STR CLIP BS 1148 STR 16R. REMOVED DAMAGED STR CLIP AND INSTALL NEW STR CLIP AT BS 1148 STR 16R.Mar 22, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00666Threshold · corrodedCORROSION (C53-113-01, 2) ON DOOR THRESHOLD STIFFENER BS 1057.5 TO 1110 WL 164 RBL 35. INSTALLED NEW DOOR THRESHOLD STIFFENER.Mar 20, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00636Clip · crackedCRACKED STR CLIP BS 420 STR 4L. REMOVED CRACKED STR CLIP, DRILLED NEW STR CLIP AND INSTALLED AT BS 420 STR 4L.Mar 20, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00635Stringer · damagedMECH DAMAGE ON STR 23L AT STA 482. REMOVED DAMAGED STR BS 482 STR 23L AND INSTALLED REPAIR PER FEDEX SRM 53-10-3.Mar 20, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00578Bulkhead Web · corrosionNR0079 AND 006, CORROSION (C53-100-0164) ON FWD SIDE OF 178 BULKHEAD RBL 21 TO 26 WL 218. *S/D* CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, BulkheadSDR 96FDEA00577Skin · creasedNR0098 AND 007, CREASE IN SKIN BS 1108 WL 208 LBL 60. REMOVED DAMAGE IN SKIN BS 1108 WL 208 LBL 60 FABRICATED AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 53-30-3.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00576Frame · damagedNR0168 AND 008, DAMAGED FRAME BS 1130 RBL 50 WL 188 UNDER FLANGE.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00574Shear Tie · corrosionNR0235 AND 010, CORROSION (C53-113-01, 2) ON SHEAR TIE BS 990 WL 158 STR 29R. REMOVED DAMAGED SHEAR TIE BS 990 WL 158 STR 29R AND INSTALLED REPAIR PER FEDEX SRM 53-10-4.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00573Frame · corrosionNR0451 AND 011, CORROSION ON FRAME BS 700 WL 155 RBL TO LBL 11.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00572Frame · corrosionNR0452 AND 012, CORROSION ON FRAME BS 700 WL 149 RBL 4.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00571Floor Beam · corrodedNR 0474 AND 013, CORROSION (C53-224-01) AND OR BARE METAL AROUND ALL NUT CLIP HOLES LOWER SURFACE BS 760 TO 848 RBL 25 WL 208 ON LONGITUDINAL FLOOR BEAM. CORROSION DAMAGE ON LONGITUDINAL FLOOR BEAM WAS FOUND OUT OF LIMITS. REMOVED DAMAGED BEAM AND INSTALLED Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00570Te Wedge · delaminationNR0480 AND 014, RT WING O/B MIDFLAP TRAILING EDGE WEDGE HAS A DISBOND 88 FROM I/B END ON UPPER SKIN.Mar 18, 1996 · N154FE · Boeing 72725 · Trailing Edge FlapsSDR 96FDEA00569Floor Beam · corrosionCORROSION (C53-224-01) ON FLOOR BEAM BS 480 LBL 39 WL 208. PERFORMED FLOOR BEAM REPAIR AT BS 480 LBL 39 WL 208 IAW 53-10-8 FEDEX 727 SRM AND ENGINEERING REQUEST.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00568Floor Beam · corrodedNR0542 AND 016, CORROSION (C53-224-01) ON LOWER SURFACE OF UPPER FLANGE OF FLOORBEAM AROUND NUTPLATE AND FASTENER HOLES, BS 1030 RBL 48 TO 60 WL 208.Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00575Forging · corroded(NR 0230 AND NR 009). CORROSION (C53-111-01 (3)) ON THE BS 950 FORGING WL 208, RBL 50. **** S/D **** REMOVED CORROSION ON THE BS 950 FORGING, WL 280, RBL 50. BLENDED DAMAGED AREA, CLEANED, TREATED AND RE-INSTALLED FASTENERS PER FEDEX EA 7-5310-28062.Mar 17, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00567Skin · damagedNR0097 AND 001, LIGHTNING STRIKE ON FASTENER HEAD BS 316 LBL 55 WL 178.Mar 15, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00566Hinge Fitting · corrodedNR0196 AND 002, LEFT O/B AILERON NR 1 HINGE FITTING IS CORRODED ON LOWER SURFACE.Mar 15, 1996 · N154FE · Boeing 72725 · AileronsSDR 96FDEA00565Skin · delaminatedNR0248 AND 003, RT WING O/B TRAILING EDGE AFT FLAP IS DELAMINATED APPROX 96 INCHES FROM I/B EDGE.Mar 15, 1996 · N154FE · Boeing 72725 · Trailing Edge FlapsSDR 96FDEA00564Bullnose · corrodedNR0323 AND 004, CORROSION ON NR 4 K-FLAP O/B BONDING JUMPER LOWER ATTACH POINT.Mar 15, 1996 · N154FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00563Chord · corrosionNR0329 AND 005, CORROSION (C53-132-02, 1) BS 870 UPPER CHORD FASTENER HEAD SHEARED AND SKIN BULGING AT RBL 52 RBL 25 TO 41 AND AT LBL 5 ON VERTICAL FLANGE.Mar 15, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00527Bullnose · corrodedCORROSION ON NR 4 K-FLAP O/B BONDING JUMPER LOWER ATTACH POINT. REMOVED CORROSION ON NR 4 K-FLAP BULLNOSE O/B BONDING JUMPER, FOUND TUBE OUT OF LIMITS PER SRM 57-50-1. BLENDED TO LIMITS PER DRAWING SR 27-57-010. CLEANED AND TREATED AREA AND REINSTALLED BONDMar 15, 1996 · N154FE · Boeing 72725 · Leading Edge DevicesSDR CA960315003Engine · duct torn(CAN) DURING A ROUTINE INSPECTION, BROKEN METAL WAS FOUND IN THE COWL OF #3 ENGINE. FURTHER INSPECTION REVEALED AN APPROXIMATELY 3 SQ.IN. HOLE AND A 8"X4" TEAR AT THE APPROXIMATELY 3 O'CLOCK POSITION OF THE BYPASS DUCT WHERE THE IGNITOR FLANGE IS MOUNTED. LOOKMar 7, 1996 · Boeing 72725 · Engine (Turbine/Turboprop)SDR 96FDEA00349Position Switch · malfunctionedLEFT I/B LEADING EDGE DEVICE NR 3 WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES WITH NO RETRACTION. REPLACED NR 3 KREUGER FLAP POSITION SWITCH PER MM 27-82-1, OPS CHECK GOOD.Feb 28, 1996 · N156FE · Boeing 72725 · Leading Edge Slat Control SystemSDR DHL9670801Frame · crackedFWD CARGO DOOR CUTOUT, FWD UPPER FRAME CRACKED AT UPPER STOP FITTING. STOP DRILLED CRACK IN FRAME PER SRM 51-10-1. FABRICATED DOUBLER REPAIR PER SRM 53-10-4, FIG 10. HEAT TREATED DOUBLER REPAIR PER BAC 5602. INSTALLED DOUBLER REPAIR PER SRM 53-10-4 FIG 10.Feb 3, 1996 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR CA960116003Valve · seized(CAN)AFTER TOUCHDOWN WHEN REVERSE THRUST WAS SELECTED THE #1 THROTTLE STUCK ON THE IDLE GATE AND THE REVERSER WOULD NOT ENGAGE. MAINTENANCE FOUND THE THRUST CONTROL SYSTEM DIRECTIONAL VALVE VERY STIFF. AFTER VALVE REPLACEMENT THE SYSTEM FUNCTIONED NORMALLY.Jan 4, 1996 · Boeing 72725 · Engine Thrust ReverserSDR DHL95708002Terminal End · burnedDURING CLIMBOUT, R-1 TOP CENTER AND TOP RIGHT CORNER OF WINDOW BEGAN TO SPARK AND SMOKE. FLIGHT RETURNED TO AIRPORT. CLEANED CONTACT BASE, REMOVED AND REPLACED TERMINAL END ON UPPER RT CORNER OF R-1 WINDOW IAW MM30-40.Nov 30, 1995 · N708DH · Boeing 72725 · Windshield/Door Rain/Ice RemovalSDR 95FDEA01698Mechanism · wornFL 31.0, MACH .84 NOTICED 10 TO 12 DEG R/YOKE DISPLACEMENT. ATTEMPTED TO TRIM RUDDER AND GOT A MOD-SEVERE BUFFET, CONTINUED AFTER SLOWING TO .80 MACH. BUFFET STOPPED WHEN EXTENDING SPEED BRAKES SLIGHTLY 1 TO 2 DEGREES. BUFFET WOULD BEGIN AGAIN AFTER RETRACTNov 7, 1995 · N507FE · Boeing 72725 · Trailing Edge Flap Control SystemSDR 95FDEA01639Rib Chord · crackedNOTED CRACK INDICATION IN FORWARD UPPER AND LOWER FASTENER HOLES AT BS 760, LBL 70.5 RIB UPPER CHORD, CRACKED IN 6 AND 12 O'CLOCK POSITIONS IN CHORD, BOTH HOLES. REPAIRED DAMAGED AREA AT BS 760, LBL 70.5, RIB UPPER CHORD IAW SB 727-57-0112, FEDEX EO 7-5710-7-Oct 30, 1995 · N152FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 95FDEA01586Stringer · corrodedSTR 28L CORRODED OUT OF LIMITS AT BS 556. REMOVED AND REPLACED FABRICATED STR SPLICE FROM BS 556 TO 607 IAW SRM 53-10-3.Oct 23, 1995 · N152FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 95FDEA01555Stringer · crackedCRACK ON STR 27L STA 427. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-3.Oct 18, 1995 · N152FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 95FDEA01554Stringer · crackedCRACKED STR 26L BS 447. REMOVED CRACKED STR SECTIONS AT BS 447 STR 26L AND REPAIRED PER FEDEX SRM 53-10-3.Oct 18, 1995 · N152FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR EISA95391Retract Mech · lack of lubeNOSE GEAR FAILED TO EXTEND NORMALLY, RECYCLED SEVERAL TIMES WITH NO GREEN LIGHT, AFTER THIRD TRY NOSE GEAR EXTENDED OK. INSPECTED AND LUBED NOSE GEAR AND ASSOCIATED LINKAGE, RAN EXTENSION AND RETRACTION PER MM 32-33-0. NO DEFECTS NOTED. (M)Oct 17, 1995 · N290NE · Boeing 72725 · Landing Gear Retraction/Extension SystemSDR EISA95401Skin · corrodedCORROSION FOUND LAP STATION 1157 TO 1183 STRINGER 20L. REMOVED CORROSION AND REPAIRED PER AAL EO 1280-011 REV A. (M)Oct 10, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95419Skin · damagedBS 1183 STRINGER 19L END FITTING HAS SEVERAL DRILL STARTS AND BROKEN SCREWS. REMOVED FITTING AND INSTALLED NEW PER SRM 51-10-2 AND SRM 51-30-4 AND SRM 51-10-1. (M)Oct 8, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95403Fitting · misdrilledFUSELAGE BS 1183, STRINGER 201 LOWER BATHTUB FITTING HAS DRILL STARTS. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-10-1 TORQUED BOLTS IAW 51-30-4. (M)Oct 6, 1995 · N290NE · Boeing 72725 · Fuselage Miscellaneous StructureSDR EISA95421Skin · crackedSKIN LAP JOINT, AT STRINGER BS 259-360, HAS 9 SINK HOLES HAVE CRACK INDICATIONS. REMOVED DAMAGE PER SRM 53-30-3 FIG 5. COMPLETED REPAIR PER SB 53-0072 REV 5 AND SRM 53-30-3. (M)Oct 5, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95406Skin · crackedRIGHT MLG STRUT DOOR AFT HINGE SKIN MISSING SEVERAL FASTENERS AND THE SKIN IS CRACKED. REMOVED DAMAGE AND REPAIRED PER SRM 52-80-2. (M)Oct 4, 1995 · N290NE · Boeing 72725 · Landing Gear DoorsSDR EISA95418Skin · crackedTWO CRACKS UPPER SKIN LAP AT STATION 520 CENTER ROW AND STATION 530 BOTTOM ROW OF STRINGER 19L. FAB DOUBLER PER EO 1280-008. (M)Oct 3, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95393Bob Weights · crackedLEFT ELEVATOR BOB WEIGHTS FOUND CRACKED. REMOVED AND REPLACED ELEVATOR BOB WEIGHTS IAW B727 MM 27-30-0. (M)Oct 3, 1995 · N300NE · Boeing 72725 · Elevator Control SystemSDR EISA95407Skin · crackedAN .75 INCH CRACK INDICATION, STRINGER 3L BS 1080. HFEL CONFIRMED CRACK LOCATED STRINGER 4L STATION 1072. REPAIRED PER SRM 53-30-3 AND SB 727-53-0072 AND AD 91-06-06. (M)Oct 2, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95411Skin · corrodedBS 660 STRINGER 22L UPPER FLANGE HAS A HOLE. REPAIRED PER SRM 53-10-3 FIG 2. (M)Sep 30, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95413Sensing Tube · bentCABIN SMOKE DETECTION SENSING TUBE IS BENT AT STATION 680 RIGHT. REMOVED DAMAGED REPOSITION TUBING PER MM 20-10-5 AND MM26-17-0 FIG 1. (M)Sep 29, 1995 · N290NE · Boeing 72725 · Smoke DetectionSDR EISA95412Skin · defectiveREPLACED INNER STRUCTURE,16 FEET LONG (P/N AE 727-1-043-13). REMOVED AND REPLACED STRUCTURE PER SRM 51-10-1 AND SRM 51-30-2. (M)Sep 29, 1995 · N290NE · Boeing 72725 · Cargo/Baggage DoorsSDR EISA95404Skin · corrosionCORROSION FOUND STRINGER 19L EXCEEDING 10 PERCENT AT BS 441. REMOVED CORROSION REPAIRED PER AAC EO 1280-0009. (M)Sep 29, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR EISA95410Skin · corrodedBS 640 STRINGER 22L UPPER FLANGE, HAS AN OPEN HOLE ADJACENT FASTENER HOLE. REPAIRED PER SRM 53-10-3 FIG 2. (M)Sep 28, 1995 · N290NE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA01444Skin · corrodedCORROSION (71C113-02) ON INSIDE SKIN AND NOSE DOOR CUT OUT FRAME BS 211, RBL 19, WL 172. REMOVED FASTENERS FOR T-CHORD EXT SKIN BS 211 FRAME AND WEB. CLEAN AND TREATED CORROSION, ALODINED, PRIMED AND RE-INSTALLED FASTENERS. REMOVED DOOR CUT OUT FRAME WEB, FSep 27, 1995 · N508FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 95FDEA01443Frame · corrodedCORROSION FOUND ON BS 740 FRAME AT LBL 3. DISCOVERED ADDITIOINAL CORROSION FROM STR 1L - 3L. MECHANICALLY REMOVED CORROSION FROM FRAME FLANGE. CUT OUT DAMAGED SKIN AT BS 742, LBL 3. REPAIRED FRAME AND SKIN PER FEDEX EA NR 7-5310-25835.Sep 27, 1995 · N508FE · Boeing 72725 · Fuselage Main, Structure
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