Boeing 727-100

Service difficulty reports · 288

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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 = '727100'
  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 06FDEA00019Stringer · dentedDENTED STRINGER AT STA 493, STR 8RT. *S/D* REPAIRED STRINGER PER SRM 53-10-3.Jan 4, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 06FDEA0018Frame · tool damageAFT CARGO COMPARTMENT, DRILL STARTS IN FRAME AT STR 23 RT AND 27 LT BS 1148 ON INBOARD FLANGE. *S/D* ALL MAINTENANCE REQUIREMENTS FOR THIS CARD ACCOMPLISHED ON CARD N00986.Jan 4, 2006 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 06FDEA0016O-Ring · leakingJUST AFTER LEVEL OFF AT 16000 EXPERIENCED COMPLETE SYS-A HYD FAILURE. QTY AND PRESSURE BOTH WENT IMMEDIATELY TO ZERO. RAN QRH CHECKLIST, TIMED SYS-A FLUID SHUTOFF SWITCHES OFF FOR 55 MIN TO LANDING. LED NR 5 AMBER AND GREEN LIGHTS ON, ALL SLATS AND LED LIGHJan 4, 2006 · N180FE · Boeing 727100 · Hydraulic System, MainSDR 06FDEA0012Floorbeam · corrodedFOUND CORROSION, STA 344 LBL 50 TO RBL 15 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. REMOVED DAMAGED SECTION OF UPPER CHORD, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8.Jan 3, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA04412Strap · corrodedN00310 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130 RBL 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130, RBL 63, WL 208, PER SRM 51-30-2.Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA04410Strap · corrodedN00312 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130 LBL. 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130, LBL 63, WL 208, IAW SRM 51-30-5, 51-30-2.Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA04414Skin · lightning strikeN00280 LIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1167, STR 13R. DETERMINED LIGHTNING STRIKE DAMAGE IN SKIN AT BS 1167, STR 13R TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A.Dec 27, 2005 · N191FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA04407Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 25 LT AND 27 LT BS 1050 ON IB FLANGE. REPAIRED DENTED FRAME BETWEEN STR 25LT AND 27LT, BS 1050 ON I/B FLANGE IAW SRM 51- 40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04406Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 24 LT AND 27 LT BS 1030 ON IB FLANGE. REPAIRED IAW SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04405Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 24 LT AND 27 LT BS 1010 ON IB FLANGE. REPAIRED PER 51-40-03 & 53-10-1.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04404Frame · dentedN00987 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 26 LT AND 27 LT BS 1148 ON IB FLANGE ** SD ** COMING.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04403Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 26 RT AND 23 RT BS, 1148 IN IB FLANGE. AFT CARGO COMPARTMENT FRAME AT BS 1148 BETWEEN STR 23R, AND 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04402Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 25 LT AND 27 LT BS 990, ON IB FLANGE. REPAIRED FRAME PER SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04242Rod · dirtyDURING TEST FLIGHT WITH GEAR HANDLE UP NOSE GEAR RED LIGHT AND RED DOORS LIGHT STAYED ON. *S/D* CLEANED DIRT FROM AND LUBRICATED NLG DOOR SWITCH ACTUATOR RODS. JACKED NOSE AND SWUNG GEAR. NLG FUNCTIONALLY TESTED GOOD. SERVICED NLG STRUT. WORK DONE PER MMDec 12, 2005 · N188FE · Boeing 727100 · Landing Gear Position and WarningSDR 05FDEA04188Skin · damagedREWORK REQUIRED, FROM NR01182. ACCOMPLISH REPAIR PER FEDEX ENGINEERING, BS 480, STR 26L-27L. *S/D* COMPLIED WITH FED EX EA 7-5330-95353, FOUND TO BE A MAJOR REPAIR.Dec 8, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA03997Repair · improperREPAIR AT BS 694, STR 19R REQUIRES ENGINEERING DISPOSITION IAW EO 7-5100-7- 5000 PT1. ACCOMPLISHED REPAIR AT BS 694 STR 19R PER FED EX E.A. 7-5330-91416.Nov 28, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA03870Odor · detectedPASSING FL 180 SMELLED FUMES IN THE COCKPIT. RAN SMOKE AND FUME CHECKLIST. RETURNED TO MEMPHIS. SMELLED LIKE BURNING RUBBER OR PLASTIC. FACT REPLACED BOTH CONDENSER BAGS AND FOUND BOTH RT AND LT AIR CYCLE MACHINES OUT OF OIL REPLACED BOTH ACM RAN BOTH PANov 18, 2005 · N198FE · Boeing 727100 · Air Distribution SystemSDR 05FDEA03858Fitting · corrodedLEFT MLG FWD TRUNNION SUPPORT FITTING O/B FLANGE, O/B SURFACE HAS SURFACE CORROSION BETWEEN -THROUGH PIN- AND LWR PORK CHOP FITTING BOLT HOLE LOCATIONS. REPAIRED L/H MLG FWD TRUNNION SUPPORT FITTING PER FED EX EA 7-5710-91408.Nov 17, 2005 · N188FE · Boeing 727100 · Main Landing GearSDR 05FDEA03795Light · inoperativeRTO FOR AFT AIRSTAIR LIGHT IAS 75 KTS. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22NOV05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. VERIFIED AFT AIRSTAIR IS CLOSED AND RED LIGHT EXTINGUISHED. COMPLIED WITH TRO HIGH ENENov 14, 2005 · N136FE · Boeing 727100 · Door Warning SystemSDR 05FDEA03767Repair · improperEXISTING EXTERNAL REPAIR ON FUSELAGE BS 620-637 STR 27R-28R. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW SRM 53-30-3 FIG 1 Nov 11, 2005 · N466FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA03562Skin · crackedBS 1352 RT SKIN CRACK AT RAIN GUTTER LOCATION. REPAIRED PER SRM 54-30-2Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA03553Failsafe · crackedBS 1010 FRAME IS CRACKED AT STRINGER 25 LEFT. REPAIRED PER SRM 51-40-3Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA03552Failsafe · crackedBS 990 FRAME IS CRACKED AT STRINGER 25 RIGHT. REPAIRED PER SRM 51-40-3Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA03551Failsafe · crackedN01348 BS 990 FRAME IS CRACKED TWO PLACES AT STRINGER 25 LT. REPAIRED PER SRM 51-40-3Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA03549Support · corrodedCORROSION AFT CARGO BAY CEILING SUPPORT BS 1107 RBL 6 WL 200. REPAIRED PER SRM 53-10-1Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA03548Shear Tie · corrodedCORROSION ON SHEAR TIE BS 990 LBL 3 WL 148. REPAIRED PER SRM 53-10-2Oct 27, 2005 · N188FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 05FDEA03504Frame · damagedUPPER LOBE INTERIOR FRAME HAS MACH DAMAGE AND OPEN HOLES BS 890 STR 9L. [OPEN]Oct 26, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA03491Skin · crackedCRACK IN FUSELAGE OUTER SKIN STA 591 STR 15R FWD UPPER CORNER OF WING L/E ILLUMINATION LIGHT CUT OUT. REPAIRED PER FED EX EA 7-5330-95384.Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA03490Floorbeam · corrodedBS 480 FLOORBEAM UPPER CHORD CORRODED AT RBL 48, WL 208. [OPEN]Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03489Intercostal · crackedN01148 CRACK BS 660 STR 2L UPPER INTERCOSTAL EXTENSION. [OPEN]Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA03487Frame · damagedN00737 FRAME BS 990 BTWN STR 22 LT- 24 LT DAMAGED. [OPEN]Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA03481Frame · dentedAFT CARGO BAY FRAME BS 1030 BETWEEN STR 26 LT AND 27 LT DENTED. FABRICATED DOUBLER CAP AT BS 1030 BTWN STR 26 AND 27 L/H USING 7075T6 .071 M590750 PER SRM 51-40-3. INSTALLED DOUBLER CAP AT BS 1030 BETWEEN STR 26 AND STR 27 LT PER SRM 51-30-2.Oct 24, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA03480Shear Tie · corrodedAFT CARGO COMP SHEAR TIE IS CORRODED BS 1130 RBL 8 WL 152. REPAIRED PER SRM 53-10-4.Oct 24, 2005 · N188FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 05FDEA03448Floorbeam · crackedN00474 E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 CRACK EXTENDING UP FROM STOP DRILL. STOP DRILLED CRACK AND REPAIRED WEB AT CRACK IN E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 IAW SRM 51-10-1 AND SRM 51-40-2Oct 18, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03442Shear Web · crackedWHILE WORKING CARD N00368 FOUND SHEAR WEB 8-5-825, RBL 65-70, WL 208 TO BE CRACKED. SHEAR WEB BS 805-825 RBL 65-70 W/L 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2. SRM 51-30-5, SRM 51-10-2.Oct 17, 2005 · N188FE · Boeing 727100 · Fuselage Main, StructureSDR 05FDEA03410Floorbeam · corrodedCORROSION BS 344 FLOORBEAM LBL 55 TO RBL 10. REPAIRED BS 344 FLOORBEAM LBL 55 TO RBL 10 PER FED-EX DWG SR 27-53-007.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03409Web · crackedWHILE WORKING N01046 FOUND WEB AT BS 344 LBL 32 CRACKED. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-02 ON WEB AT BS 344 LBL 32.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA03408Floor Panel · corrodedCORROSION ON MAIN CARGO DECK FLOOR PANEL WEB AT BS 1150, RBL 60, WL 208. CUT OUT DAMAGE FLOOR WEB AT BS 1150, RBL 60, WL 208 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Floor PanelSDR 05FDEA03407Web · gougedHAYES MOD WEB GOUGED AT 9 PLACES BETWEEN STR 5L AND STR 13L BS 620. REPAIRED GOUGES STR 5L AND 13L, BS 620 HAYES MOD WEB PER SRM 53-10-2, 51-40-2, 51-30- 2.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA03406Web · gougedHAYES MOD WEB GOUGED AT BS 640L AT STR 12L AND 14L.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA03405Stringer · damagedUPPER LOBE INTERIOR SIDE OF STRINGER IS DAMAGED BS 782 STR 4L. REPAIRED STRINGER AT B.S. 782 STR 4L PER SRM 53-10-1.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 05FDEA03404Floorbeam · corrodedCORROSION BS 328 FLOORBEAM AT FASTENER HOLES. CORROSION ON FLOORBEAM AT B.S. 328 LBL 22 WAS OUT OF LIMITS REPAIRED FLOORBEAM PER FED EX EA 7-5310-91401.Oct 12, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03393Shear Tie · corrodedAFT CARGO COMP SHEAR TIE IS CORRODED BS 1110 RBL 8 WL 150.Oct 11, 2005 · N188FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 05FDEA03392Floorbeam · corrodedCORROSION BS 360 FLOORBEAM BL 0. REJECTED BECAUSE CORROSION AND BARE METAL STILL PRESENT ON BOTTOM SIDE OF UPPER CHORD AND BL 0. REPAIRED PER SRM 53-10-8.Oct 11, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03391Floorbeam · corrodedCORROSION AFT CARGO BAY FLOORBEAM LWR CHORD BS 1110 RBL 4 - 24 WL 200. CUT OUT DAMAGE ON LWR FLANGE OF BS 1110 FLOORBEAM RBL 2-RBL 26. FABRICATED AND INSTALLED REPAIR IAW FEDEX SR DRAWING SR 27-53-034E.Oct 11, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03341Stringer Clip · missingSTRINGER CLIP MISSING AT BS 600 STR 4R. INSTALLED STRINGER CLP AT BS 600 STR 4R PER SRM 51-30-2.Oct 10, 2005 · N188FE · Boeing 727100 · Fuselage Main, Attach FittingsSDR 05FDEA03255Frame · corrodedE & E BAY CORROSION ON FRAME SPLICE ANGLE AFT SIDE BS 460 STR 26L. REMOVED CORROSION ON FRAME SPLICE FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE ANGLE & INSTALLED ALL WORK DONE IAW SRM 53-10-1, 51-40-04, 51-30-2.Oct 6, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA02746Skin · damagedEXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166-1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED EX EA 7-5330-91350.Sep 4, 2005 · N192FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 05FDEA02661Bracket · crackedCOVE PANEL BRACKET IS BROKEN ON LOWER WING PANEL BELOW NR 3 SPOILER. REMOVED AND REPLACED 3 EA BRACKET P/N 65-21658Y29, 65-21658-27, AND 65-21658Y30, AND 1 EA ROD P/N 69-17911-18 IAW SRM 51-30-2.Aug 25, 2005 · N136FE · Boeing 727100 · Wing, Attach FittingsSDR 05FDEA02294Channel · crackedRIGHT WING TRAILING EDGE AT AFT SPAR AREA 3 EA CLOSE OUT PANEL SUPPORTS ARE CRACKED LOCATED UNDER NR 12 & 13 SPOILER PANELS. REMOVED AND REPLACED 3 EACH CHANNEL SUPPORTS IAW SRM 51-30-2.Aug 6, 2005 · N107FE · Boeing 727100 · Wing Miscellaneous Structure
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