Boeing 727-233

Service difficulty reports · 3,034

Newest first. General aviation reporting is voluntary.

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 = '727233'
  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 96FDEA00079Skin · damagedBS 1073 STR 19 TO 20L THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.Jan 23, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00127Frame · dentedDENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO 44 WL 160 IAW FEDEX SRM 51-40-3.Jan 22, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00113Skin · dentedFIVE DENTS IN SKIN STA 1050 TO 1056, STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3.Jan 22, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00115Stringer · damagedGOUGE ON STRINGER AT BS 460 STR 3R. REMOVED DAMAGED SECTION STR 3R BS 460, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.Jan 20, 1996 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 96FDEA00114Stringer · damagedMECHANICAL DAMAGE IN HAT SECTION OF STRINGER, AT BS 620 STR 4R. REMOVED DAMAGED SECTION STRINGER 4R BS 620, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.Jan 20, 1996 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 96FDEA00112Skin · creasedBS 1030 TO 1050, STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050, STR 20 TO 21L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.Jan 20, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00111Skin · creasedBS 1973 STR 19 TO 20L, THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.Jan 20, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00129Skin · damagedAREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 498 AND 503 BETWEEN STR 26 TO 27R, MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITH LIMITS EXCLUDING TWO AREAS. Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00095Seat Track · corrodedCORROSION (C53-224-01), ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED SECTION OF TRACK, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-5.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00094Skin · damagedAREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT TO RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 496 AND 503 BETWEEN STR 26-27R, MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITHIN LIMITS EXCLUDING 2 AREAS. ONE Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00093Frame · gougeFOUND GOUGE IN FRAME STA 360 WL 156 LBL 40, BETWEEN STR 24 TO 25 LT, E-BAY. REMOVED DAMAGE AND FABRICATED PART. REPAIRED PER SRM 51-40-3 AND 53-10-2.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00092Te Skin · delaminatedLT WING I/B FOREFLAP I/B TRAILING EDGE HAS DELAMINATED AREA, MARKED. REPAIRED PER SRM 51-40-6.Jan 19, 1996 · N273FE · Boeing 727233 · Trailing Edge FlapsSDR 96FDEA00091Skin · delaminatedLT WING O/B AFT FLAP DELAMINATED 14 INCHES FROM O/B END T/E. REPAIRED PER SRM 51-40-06.Jan 19, 1996 · N273FE · Boeing 727233 · Trailing Edge FlapsSDR 96FDEA00090Te Wedge · delaminatedRT WING O/B AILERON T/E WEDGE DELAMINATED AT O/B END. REPAIRED PER SRM 51-40-6.Jan 19, 1996 · N273FE · Boeing 727233 · AileronsSDR 96FDEA00089Skin · disbondedRT WING I/B FOREFLAP I/B END HAS DISBONDED RUBSTRIP UPPER SURFACE. REPAIRED PER SRM 51-40-06.Jan 19, 1996 · N273FE · Boeing 727233 · Trailing Edge FlapsSDR 96FDEA00087Frame · dentedDENT IN FRAME BS 500 LBL 34 TO 46 WL 160.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00086Stringer · corrosionCORROSION (53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 96FDEA00085Beam · corrosionCORROSION (C53-221-01), ON 25G BEAM AT BS 268 LBL 7 WL 08.1. REMOVED AND REPLACED 25G BEAM PER SRM 53-10-01.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00083Frame · dentedDENTS IN FRAME BS 500 RBL 34 TO 44 WL 160. CUT OUT DAMAGE REPAIRED FRAME BS 500 RBL 34 TO 44 WL 160 PER FEDEX SRM 51-40-3.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00082Frame · dentedDENTS IN FRAME BS 700 LBL 34 TO 44 WL 160. REMOVED DAMAGE AND FABRICATED REPAIR PARTS PER SRM 51-40-3.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00081Frame · dentedDENTS IN FRAME BS 680 LBL 34 TO 45 WL 160. CUT OUT DAMAGE ON FRAME BS 680 LBL 34 TO 45 WL 160, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 51-40-3.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00080Skin · damagedBS 1030 TO 1050 STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050 STR 20 TO 21L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.Jan 19, 1996 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00131Frame · dentedDENTS IN FRAME BS 520 LBL 37 TO 46 WL 160. DENTS IN FRAME AT BS 520 LBL 37 TO 46 WL 160 WERE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3.Jan 18, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00088Frame · dentedDENT IN FRAME BS 500 LBL 34 TO 46 WL 160. CUT OUT DENT, FABRICATED REPAIR DOUBLER, CLEANED, TREATED PART AND FRAME. INSTALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3.Jan 18, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00070Frame · dentedDENTS IN FRAME BS 580, LBL 37 - LBL 46, WL 160. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 580, LB 37 - LB 46, WL 160 PER FEDEX SRM 51-40-3.Jan 18, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00069Frame · dentedDENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO RBL 44 WL 160 IAW FEDEX SRM 51-40-3.Jan 18, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00068Frame · gougedGOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14. GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14 WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND WAS REPAIRED PER FEDEX SRM 51-40-3.Jan 18, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00062Frame · dentedDENTS IN FRAME BS 600 LBL 34 TO 46 WL 160. REPAIRED DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160 PER FEDEX SRM 51-40-3.Jan 17, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00061Frame · gougeGOUGE IN FRAME AT BS 720B LT BETWEEN STR NR 14 TO NR 15, WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-40-3. REMOVED AND REPLACED FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3.Jan 17, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00063Frame · dentedDENTS IN FRAME BS 660 LBL 34 TO 46 WL 160. REPAIRED DENTED FRAME BS 660 LBL 34 TO 46 WL 160 IAW FEDEX SRM 51-40-3.Jan 16, 1996 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01894Dnlock Bushing · wornLANDING AT MEM, PUT DOWN GEAR; MAINS GOOD BUT NOSE GEAR KEPT RED LIGHT AND NO GREEN LIGHT. RECYCLED GEAR, GOT GREEN MAINS AGAIN, AND RED NOSE GEAR LIGHT. ON GO AROUND, NOSE GEAR AND LIGHTS WENT GREEN APPROX 1 MINUTE AFTER RECYCLED GEAR. REPLACED BUSHING ON NDec 13, 1995 · N222FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 95FDEA01886Manifold Vlv · wired closedDIVERTED TO MCI DUE TO NR 2 FUEL TANK WITH NO CROSSFEED. ENG BURN ONLY. FOUND NR 2 MANIFOLD VALVE DEFERRED ON LOG PAGE 345931. ALSO, FOUND WIRED IN CLOSED POSITION. REPOSITIONED VALVE TO OPEN POSITION AND SECURED MANUAL HANDLE WITH SAFETY WIRE. OKAY TO CODec 9, 1995 · N262FE · Boeing 727233 · Aircraft Fuel Distribution SystemSDR 95FDEA01841Skin · damagedA/C STRIKE IN FRONT OF CARGO DOOR, APPROX 12 INCHES LONG ON FUSELAGE. REMOVED GILLINER TO ACCESS BACKSIDE OF DAMAGE. REPAIRED PER EA NR 7-5330-26264 WITH FILLER, DOUBLER AND HI-LOKS.Dec 2, 1995 · N258FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01672Skin · corrodedCORROSION ON INTERIOR SHIP SURFACE AT BS 703, BL O AROUND NUTPLATES. CUT OUT CORRODED SKIN THAT WAS BEYOND LIMITS PER FEDEX SRM 53-30-4, INSTALLED DOUBLER PER FEDEX SRM 53-30-8, CLEANED AND TREATED AREA.Nov 3, 1995 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01675Drive Motor · leakingLOSS OF SYSTEM-A OCCURRED 30 MINUTE AFTER TAKEOFF. RAN CHECK LIST VERIFIED SYSTEM-A LEAK. SHUT-OFF BOTH SYSTEM-A FLUID SHUT-OFF SWITCHES. LEAK/FLUID LOSS STOPPED WITH LESS THAN 1 GALLON. REMOVED 40 DEGREE FLAP STOP, REMOVED AND REPLACED HYDRAULIC FLAP DRIVNov 2, 1995 · N219FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 95FDEA01614Skin · corrosionCORROSION ON INTERIOR SKIN SURFACE AT BS 703, BL ZERO AROUND NUTPLATES. CUT OUT CORRODED SKIN THAT WAS BEYOND LIMITS PER FEDEX SRM 53-30-4. INSTALLED DOUBLER PER FEDEX SRM 53-30-3. CLEANED AND TREATED ALL AREAS.Oct 27, 1995 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01594Apu · fireGROUND CREW REPORTED, APU W/N LIGHT OFF OR SHUTDOWN, RESIDUAL FUEL IGNITED CAUSING FIRE AND FIRE BOTTLE DISCHARGED. STARTED APU 3 TIMES, OPS CK GOOD. APU SHUTDOWN NORMALLY WITH MASTER SW OR FIRE HANDLE. SUSPECT NO LIGHT ON APU WAS CAUSED BY COLD SOAKED APU.Oct 25, 1995 · N272FE · Boeing 727233 · Airborne Auxiliary Power Unit (APU) SystemSDR 95FDEA01546Floorbeam · corrodedCORROSION ON LONGITUDINAL FLOORBEAM AT BS 766 TO 852 LBL 24 WL 208. FOUND CORROSION BEYOND LIMITS PER FEDEX SRM 53-10-1. REMOVED DAMAGED BEAM FABRICATED AND INSTALLED NEW BEAM PER FEDEX SRM 53-10-2 AND FEDEX MM 28-11-0.Oct 16, 1995 · N265FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01537Skin · dentedNR 3 CARGO DOOR OUTER SKIN LWR FWD CORNER IS DENTED BEYOND ALLOWABLE LIMITS OF FEDEX SRM 52-00-2. REPAIRED LWR FWD CORNER ON NR 3 CARGO DOOR PER FEDEX SRM 52-00-3.Oct 11, 1995 · N165FE · Boeing 727233 · Cargo/Baggage DoorsSDR 95FDEA01532Seat Track · corrodedREMOVED CORROSION AROUND FASTENER HOLES, FLOOR PANEL. THE CORROSION WAS FOUND UNDER SEAT TRACK. REMOVED SEAT TRACK, ORIGINAL THICKNESS ON LONGITUDINAL BEAM .090 UPPER HORIZONTAL FLANGE, FOUND TO BE OUT OF LIMITS MAX ALLOWABLE 10 PERCENT. REMOVED FROM .017 TOct 10, 1995 · N265FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01515Skin · crackedCRACK FOUND IN SKIN AT BS 1218 WL 138.5 RBL 10. STOP DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER ON SKIN, ALL WORK DONE PER FEDEX SRM 53-30-2 AND 51-10-1.Oct 9, 1995 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01514Skin · damagedWORKING FASTENERS AT BS 1342.4 STR 8 TO 14L. CUT OUT DAMAGED SKIN, FABRICATED FILLERS AND DOUBLER, ALODINED AND PRIMED. SEALED REPAIR PARTS AND INSTALLED WITH FASTENERS WET WITH SEALANT PER FEDEX SRM 54-30-3.Oct 9, 1995 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01513Skin · damagedWORKING FASTENERS AT BS 1342.4 STR 8 TO 12R. CUT OUT DAMAGE SKIN, FABRICATED FILLERS AND DOUBLERS. ALODINED AND PRIMED SEALED AND INSTALLED WITH FASTENERS WET WITH SEALANT PER FEDEX SRM 54-30-3.Oct 9, 1995 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01507Drive Motor · leakingDURING CLIMB, ENGINEER NOTICED A-SYS HYD DECREASING, PERFORMED IMMEDIATE ACTION, A-SYS KEPT DECREASING. PERFORMED HYD LEAK CKLIST AND RETURNED TO MEM. RAN WITH FLUID SHUT-OFF VALVES CLOSED FOR 15 MINS. FOUND RIGHT O/B MOTOR SEAL BLOWN, REPLACED MOTOR AND A-Oct 5, 1995 · N280FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 95FDEA01465Accessory Unit · failedLANDING GEAR WON'T RETRACT. TROUBLESHOT IAW MM 33-31-11 PG 101 AND 501. TRACED PROBLEM TO LANDING GEAR ACCESSORY UNIT. REMOVED AND REPLACED MLG ACCESSORY UNIT, OPS CHECKED GOOD AS PER MM.Sep 30, 1995 · N263FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 95FDEA01375Shear Tie · corrodedCORRODED SHEAR TIE AT BS 970 RBL 8 WL 138. FABRICATED AND INSTALLED SHEAR TIES PER SRM 53-10-4.Sep 18, 1995 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA01374Skin · corrodedCORROSION ON UPPER SKIN OF WING CENTER SECTION BS 826 BETWEEN STR 80 TO 70 RBL 50. BLENDED CORROSION NDI VERIFICATION OF CORROSION REMOVAL. REMOVAL OF MATERIAL WITHIN LIMITS, WORN PER EA 7-5710-25770.Sep 18, 1995 · N268FE · Boeing 727233 · Wing, Plate/SkinSDR 95FDEA01373Floorbeam · corrodedCORROSION ON FLOORBEAM BS 312 LBL 4, 19, 45 WL 208 AROUND NUTPLATE HOLES. REPAIRED CORRODED AREA ON FLOORBEAM BS 312 LBL 19 WL 208 AROUND NUTPLATE HOLES PER FEDEX 53-10-8 FIG 7. REMOVED CORROSION ON BS 312 FLOORBEAM LBL 4 AND 45 WL 208, FOUND TO BE WITHIN LISep 18, 1995 · N268FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01372Keel Beam · corrodedCORROSION IN THE AFT CARGO BAG, CORROSION ON KEEL BEAM STR 29L BS 950E PLUS 5 TO 950E PLUS 13 AND AT BS 950L PLUS 12. REMOVED CORROSION AND TREATED AREA PER EA 7-5310-25771 AND EWO 95-3089.Sep 18, 1995 · N268FE · Boeing 727233 · Fuselage Main, KeelSDR 95FDEA01371Keel Beam · corrodedCORROSION IN THE AFT CARGO BAG, CORROSION ON O/B FLANGE OF STR 29R KEEL BEAM AT BS 950F TO 970 BS 976, 982, 989 AND 990 TO 1000. REMOVED AND REPLACED KEEL BEAM PER FEDEX EA 7-5310-25768 AND EWO 95-3091.Sep 18, 1995 · N268FE · Boeing 727233 · Fuselage Main, Keel
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