Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  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 03FDEA00502Panel · crackedCABIN BS 1176.9 LEFT SIDE GILLINER CLOSE OUT CRACKED. REPAIRED CLOSEOUT IAW FED EX SRZ 25-016A.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00501Duct · crackedOVERHEAD CABIN AIR CONDITIONING DUCT STA 450 TO 670 HAS NUMEROUS AREAS OF DELAMINATION AND CRACKING. *S/D* REPAIRED OVERHEAD A/C DUCT IAW BOEING CMM 25-00-67.Apr 17, 2003 · N218FE · Boeing 727200 · Air Distribution SystemSDR 03FDEA00500Fairing · looseRIGHT OUTBOARD MIDFLAP INBOARD JACKSCREW FAIRING HAS A LOOSE SKIN AND DOUBLER ON SIDE. *S/D* RE-ATTACHED LOOSE DOUBLER WITH 2 EA RIVETS THAT WHERE LOOSE IAW BOEING SRM 51-30-02.Apr 17, 2003 · N218FE · Boeing 727200 · Trailing Edge FlapsSDR 03FDEA00498Cover · gougedLEFT WING INBOARD FORE FLAP UPPER SURFACE GOUGED UNDER NR 2 GROUND SPOILER. REMOVED AND REPLACED COVER PLATE IAW BOEING 727-200 SRM 51-30-02.Apr 17, 2003 · N218FE · Boeing 727200 · Wing Miscellaneous StructureSDR 03FDEA00496Skin · damagedNR 2 ENGINE RIGHT AFT NACELLE SKIN LOWER AFT CORNER BENT AND CHAFED. *S/D* REPAIRED BENT CORNER AND CHAFED EDGE IAW BOEING 727-200 SRM 54-10-03.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00495Skin · crackedNR 2 ENGINE LEFT AFT NACELLE LOWER FORWARD CORNER SKIN HAS A CRACK AND CHAFING. REPAIRED NR 2 ENGINE COWLING FWD LOWER CORNER IAW BOEING 727-200 SRM 54-10-03.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00494Skin · chafedNR 2 ENGINE FORWARD COWLING LOWER AFT CORNER INTERIOR SKIN CHAFED. *S/D* REPAIRED SKIN IAW BOEING 727-200 SRM 54-30-01.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00492Structure · bentNR 2 ENGINE RIGHT FORWARD COWLING RAIN GUTTER BENT. REPAIRED NR 2 ENGINE RIGHT HAND COWLING RAIN GUTTER IAW BOEING 727-200 SRM 51-40-01.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon Miscellaneous StructureSDR 03FDEA00491Web · crackedAFT AIRSTAIR AREA AT STA 1223 RIGHT SIDE UPPER LIGHTENING HOLE IS CRACKED IN TAIL COMPARTMENT VERTICAL WEB. REPAIRED CRACK IN LIGHTENING HOLE WEB BY INSTALLING A DOUBLER PLATE IAW BOEING 727-200 SRM 53-10-02.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00490Cover · delaminatedNOSE LANDING GEAR METERING VALVE COVER HAS DELAMINATION ON UPPER SURFACE. REPAIRED NOSE LANDING METERING VALUE COVER IAW BOEING CMM 25-00-67.Apr 17, 2003 · N218FE · Boeing 727200 · Nose/Tail Landing GearSDR 03FDEA00489Panel · crackedBENEATH CIRCUIT BREAKER PANEL FLIGHT CONTROL, APU, HYDRAULIC SYSTEM COVER PANEL IS CRACKED. *S/D* REPAIRED CIRCUIT BREAKER PANEL IAW BOEING CMM 25-00-61.Apr 17, 2003 · N218FE · Boeing 727200 · Flight Compartment EquipmentSDR 03FDEA00488Panel · crackedTHE COVER PANEL OVER THE CAPTAINS RT RUDDER PEDAL IS CRACKED. REPAIRED COVER PANEL IAW BOEING CMM 25-00-67.Apr 17, 2003 · N218FE · Boeing 727200 · Flight Compartment EquipmentSDR 03FDEA00486Frame · crackedNR 1 ENGINE UPPER NACELLE SKIN HAS CRACK FORWARD OF PIN LATCH CUTOUT AREA. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BOEING 727 SRM 51-30-2.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Frame/Spar/RibSDR 03FDEA00485Doubler · looseLOWER FUSELAGE JUST FORWARD OF AIRSTAIR RIGHT SIDE HAS LOOSE DOUBLER. *S/D* FABRICATED REPLACEMENT DOUBLER IAW BOEING 727 SRM 51-51-2 AND 51-30-2 AND 51-20-1.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00484Doubler · looseLOWER FUSELAGE JUST FORWARD OF AFT AIRSTAIR LEFT SIDE HAS A LOOSE DOUBLER. *S/D* REMOVED AND REPLACED REPAIR DOUBLER IAW BOEING 727 SRM 53-30-3.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00483Skin · damagedNR 1 ENGINE UPPER NACELLE FORWARD UPPER CORNER SKIN SEPARATED. REMOVED AND REPLACED REPAIR DOUBLER IAW BOEING 727 SRM 51-30-2.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00482Frame · gougedNR 3 ENGINE NACELLE HAS A GOUGE AT FRAME NR 7. REPAIRED COWLING FRAME IAW BOEING 727 SRM 54-10-2 FIGURE 5.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Frame/Spar/RibSDR 03FDEA00480Skin · dentedNR 3 ENGINE UPPER NACELLE EXTERIOR SKIN HAS 1 DENT APPROXIMATELY 24 INCHES FROM AFT EDGE. INSTALLED FLUSH REPAIR IAW BOEING 727 SRM 54-30-2.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00479Skin · damagedNR 3 ENGINE UPPER COWLING LOWER EDGE SKIN SEPARATED, BENT AND CHAFED AT NR 3 FRAME.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00478Frame · chafedNR 3 ENGINE UPPER COWLING NR 5 UPPER LATCH FRAME STIFFENER HAS CHAFING CONDITION.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Frame/Spar/RibSDR 03FDEA00477Warning Light · false activationDURING DESCENT INTO MEM, FIRE WARNING BELL CAME ON 3 TIMES. DURATION WAS 2-3 SECONDS, DURING THIRD INCIDENT NR 1 FIRE LIGHT ILLUMINATED BRIEFLY. LIGHT TESTED GOOD DURING TEST. REMOVED AND REPLACED ENGINE FIRE DETECTION CONTROLLER, PER MM 26-11-000-4, OPS CHApr 17, 2003 · N212FE · Boeing 727200 · Fire DetectionSDR 03FDEA00476Skin · chafedNR 3 ENGINE LOWER COWLING UPPER FRAME NEXT TO OIL TANK ACCESS DOOR HINGE HAS CHAFING CONDITION.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00475Skin · dentedNR 3 ENGINE LOWER COWLING EXTERIOR SKIN FORWARD MID AND AFT HAS 7 DENTS.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00474Frame · chafedNR 3 ENGINE COWLING FRAME NR 5 HAS A HOLE AND CHAFING CONDITION.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Frame/Spar/RibSDR 03FDEA00473Panel · tornMAIN CABIN STA 400 LEFT SIDEWALL PANEL IS TORN IN UPPER AREA.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00472Floor Panel · damagedAFT CARGO PIT STA 1030 TO 1070 FORWARD CENTER FLOOR PANEL HAS SEVERAL GOUGES AND A PREVIOUS REPAIR.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Floor PanelSDR 03FDEA00471Floor Panel · damagedAFT CARGO PIT AT STA 960E TO 990 FORWARD FLOOR PANEL HAS A HOLE.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Floor PanelSDR 03FDEA00470Structure · debondedLEFT OUTBOARD AILERON TAB I/B AFT CORNER DISBONDED.Apr 17, 2003 · N218FE · Boeing 727200 · Aileron TabsSDR 03FDEA00499Structure · tornLEFT WING AILERON TRIM TAB INBOARD UPPER SURFACE DISBONDED AND TORN ON HONEYCOMB MATERIAL.Apr 17, 2003 · N218FE · Boeing 727200 · Wing Main, Frame StructureSDR 03FDEA00487Skin · damagedNR 1 ENGINE UPPER NACELLE EXTERIOR SKIN HAS A NICK AT BOTTOM OF AFT PIN LATCH CUTOUT.Apr 17, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00467Motor · failedAFTER T/O FLAP RETRACTION - OUTBOARD T/E FLAPS STAYED AT 5 DEG WHEN FLAPS WERE RETRACTED TO 2 DEGREES. USED ALT FLAP MASTER SWITCH TO RETRACT FLAPS PER QRH PROCEDURE. PERF T/S AND FOUND OUTBOARD FLAP STUCK FROM 5 TO 2, RESET USING ALTERNATE. COULD NOT GET IApr 17, 2003 · N220FE · Boeing 727200 · Trailing Edge Flap Control SystemSDR 03FDEA00468Skin · dentedRIGHT WING LEADING EDGE HAS A DENT ABOUT 6 FEET OUTBOARD OF THE FUSELAGE.Apr 17, 2003 · N218FE · Boeing 727200 · Leading Edge DevicesSDR 03FDEA00469Floor Panel · damagedA .75 X 3.5 INCH HOLE IN FLOOR OF AFT LOWER CARGO COMPARTMENT STATION 1020.Apr 17, 2003 · N218FE · Boeing 727200 · Fuselage Floor PanelSDR 03FDEA00455Skin · corrodedN00344 CORROSION FWD CARGO BAY INNER SKIN AT B/S 720B+12 RBL 25. REPAIRED EXTERNAL SKIN AT B.S. 720B+12", RBL 25, WL 148 IAW SRM 53-30-3 AND FED EX E.A. 7-5330-54470.Apr 16, 2003 · N486FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00457Stringer · corrodedSTRINGER HAS CORROSION ON STR 29L BS 950E TO BS 1020. REMOVED AND REPLACED STR 29L (KEEL BEAM) IAW FED EX E.A. 7-5310-69472.Apr 16, 2003 · N486FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00452Stringer · corrodedSTRINGER HAS CORROSION (C53-113-01-2) 28L BS 950E+3 LBL 16 WL 150. REPAIRED STR. 28L B.S. 950E+3 LBL1 6 WL 150 IAW SRM 53-10-3.Apr 16, 2003 · N486FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00466Skin · chafedNR 3 ENGINE NACELLE SKIN CHAFED AROUND NR 4 INBOARD LATCH. *S/D* REPAIRED SKIN AT NR 4 LATCH IAW BOEING 727-200 SRM 54-10-03.Apr 16, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Main FrameSDR 03FDEA00465Skin · gougedNR 3 ENGINE UPPER NACELLE EXTERIOR SKIN GOUGED NEXT TO NR 1 LATCH. *S/D* REPAIRED NR 3 ENGINE NACELLE IAW BOEING 727-200 SRM 54-30-03.Apr 16, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00464Skin · crackedNR 3 ENGINE NACELLE INBOARD SKIN CHAFED AND CRACKED 1 INCH LONG. *S/D* REMOVED AND REPLACED DAMAGED LONGERON IAW BOEING 727-200 51-30-02.Apr 16, 2003 · N218FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA00463Stiffener · gougedLEFT WING NR 3 FLAP TRACK MOVEABLE FAIRING I/B FORWARD INTERNAL STIFFENER GOUGED. *S/D* REMOVED AND REPLACED RIB STIFFENER IAW BOEING 727-200 SRM 57-20-03.Apr 16, 2003 · N218FE · Boeing 727200 · Wing Miscellaneous StructureSDR DHL2003741546Floorbeam · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, FLOORBEAM AT BS 1070 LWR FLANGE FWD SIDE AT APPROXIMATELY LBL 14.0 CORRODED. DAMAGE FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 2. CUT OUT DAMAGED AREA DIMENSIONS 2 X 4 INCHES ON LWR FLANGES IAW B-727 SRM 53-10-8 FIG Apr 16, 2003 · N741DH · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00454Skin · corrodedCORROSION (C53-113-01-2) ON INNER SKIN SURFACE BS 950F+1 TO 8 LBL-16. BLENDED SKIN OUT OF LIMITS PER SRM 53-30-1. SKIN REPAIR TO BE ACCOMPLISHED ON NR00317 FUSELAGE 5093.Apr 16, 2003 · N486FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00453Frame · corrodedCORROSION AT STA 990, LBL 7, WL 140 FRAME HAS CORROSION. CORROSION ON FRAME BS 990 LBL 7 WL 140 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FRAME IAW SRM 53-10-4 FIG 13.Apr 16, 2003 · N486FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00462Skin · dentedRIGHT FUSELAGE STA 277 FORWARD TOILET SERVICE PANEL SKIN HAS DEEP DENT. REPAIRED IAW FEDEX EA 5330-69463Apr 16, 2003 · N218FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00456Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1130 BETWEEN LBL 45 TO RBL 45 WL 200.Apr 16, 2003 · N486FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00458Frame · crackedCRACK AT LIGHTENING HOLE IN HORIZONTAL FRAME AT BS 1183 RBL 44 WL 194.0. FABRICATED AND INSTALLED FRAME SECTION IAW BOEING 727-200 SRM 51-30-2 PG 2 AND 3 ITEM B AND 51-30-2 PG 8 ITEM D.Apr 16, 2003 · N218FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00449Bulkhead · crackedCRACK IN LEFT WHEEL WELL STATION 870 BULKHEAD SKIN WEB. ** S/D ** REPAIRED CRACK IAW FEDEX EA 7-5310-69465Apr 15, 2003 · N218FE · Boeing 727200 · Fuselage Main, BulkheadSDR 03FDEA00450Bulkhead · crackedCRACKS IN RIGHT WHEEL WELL, 870 BULKHEAD SKIN WEB. REPAIRED CRACK IAW FEDEX EA 7-5310-69465Apr 15, 2003 · N218FE · Boeing 727200 · Fuselage Main, BulkheadSDR 03FDEA00441Frame · damagedBS 560 FRAME AND SHEAR TIE HAVE TWO FASTENER HOLES THAT HAVE BEEN DRILLED UP INTO THE VERTICAL PORTION OF THE FRAME LBL 12 WL 148. REPAIRED B.S. 560, LBL 12, W.L. 148 SHEAR TIE IAW SRM 53-10-4 FIG 13 AND FED EX E.A. 7-5310-54467.Apr 15, 2003 · N486FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00444Tripler · wornCOMPLY WITH EA 7-5330-68778; TRIPLER SURROUNDING MAIN CARGO DOOR HAS WEAR, REWORK AS INSTRUCTED. FACT 15APR03 10:55 BFM R, COMPLIED WITH EA 7-5330-68778 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR, P/N 53FX1301-9/-7 (AD 2002-16-19).Apr 15, 2003 · N282FE · Boeing 727200 · Fuselage Main, Plate/Skin
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