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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 05FDEA02087Compressor · stalledDURING T/O THROTTLE UP THE NR 3 ENG HAD A COMPRESSOR S TALL . RAN NR 3 ENG UP INDIVIDUALY AND AT A VERY LOW EPR NR 3 EXPERIENCED ANOTHER COMPRESSOR STALL. WINDS CALM. INSP INLET & EXH AREA. ALL NORMAL CKED FOR BLEED VALVE OPERATION, NORMAL, HEARD ALL 3 CSDR 05FDEA01746Indicator · false indicationNR 3 FUEL GAGE ERRONEOUS INDICATION, AT T/O SHOWED 11.1, SHORTLY INTO FLIGHT GAGE DROPPED 5K LBS. AT CRUISE FLT BOOST PUMPS ILLUMINATED. UPON LANDING AT KFSD, NR 3 FUEL QTY SHOWED EMPTY. ACFT RELEASED FOR SERVICE PER MEL/CDL: 28-11-02. FOUND NR 3 INDICATOR VESDR 05FDEA01745Hydraulic System · leakingAT ROTATION A-SYS HYD FLUID WENT TO ZERO, RAN QRH, KEPT GEAR DOWN AND FLAPS 15, HAD A-SYS FLUID SHUT OFF SWITCHED OFF 23 MIN. DECLARED EMERGENCY. R & R INBOARD FLAP FLOW LIMITING VALVE PER MM. R & R NR 1 & 2 ENGINE PUMP CASE DRAIN FILTERS PER MM. R & R BOTHSDR 05FDEA00647Control System · out of adjustAIRFRAME VIB INTERMITTENT DURING CLIMB AND CRUISE. IN CLEAN CONFIG NO NOTICEABLE VIB DURING DESCENT OR CONFIG CHANGES FOR LANDING, DURING CRUISE ENG CHANGES AND SPOILER DEPLOYMENT HAD NO EFFECT. FOUND LEFT AND RIGHT TRAILING EDGE FLAP DROOP ADJ OUT OF LIMITSSDR 05FDEA00483Stiffener · crackedDURING B-CHECK, STIFFENER FITTING BELOW "S" DUCT CRACKED AND FRAMING STRUCTURE FOR "S" DUCT CORRODED, BOTH AT BS 1342 BOTH ON RT SIDE REF EA NR7-5310-87123 FOR FERRY FLT APPROVAL.SDR 05FDEA00093Fairing · missingON ARRIVAL FOUND AFT CARGO DOOR MOVABLE FAIRING MISSING FROM AIRCRAFT. INSTALLED AFT CARGO DOOR MOVABLE FAIRING PER 727-100 MM 52-33-00-4. OPS CHECK GOOD.SDR 05FDEA00092Rib · crackedSTABILIZER-ELEVATOR HINGE SUPPORT RIB INSPEC - S/B 727-55A0091 R1 COMPLY WITH EO 7-5510-7-5001. FOUND CRACK IN RIB AT ELEVATOR STA 50.50 DURING INSPECTION IAW EO 7-5510-5001. REMOVED AND REPLACED RIB IAW EO 7-5510-5001.SDR 05FDEA00081Actuator · leakingUPON GEAR RETRACT AFTER T/O RED RT GEAR LIGHT ILLUMINATED & AMBER RT MLG DOOR LIGHT ON S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO DOWN POS. 3 GREEN DOWN/LOCKED INDICATION & NO RED RT AMBER LIGHTS RAISED GEAR HANDLE AND RED RT GEAR LIGHT AND RT MLG DOOR LIGHT SDR 05FDEA00020Splice · crackedSTRINGER 4R SPLICE IS CRACKED ON EACH SIDE OF FRAME AT STA 480. REMOVED AND REPLACED STRINGER 4R SPLICE AT STA 480 IAW SRM 51-10-1.SDR 05FDEA00019Rib · crackedSECOND INBOARD RIB IS CRACKED IN LEADING EDGE OF NR 5 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-10-1.SDR 04FDEA03505Rib · crackedRIGHT HORIZONTAL STAB ELEVATOR STATION 17.20, INBOARD RIB CRACK RUNS FROM RIVET ON UPPER. REMOVED RIB IAW SRM 51-30-2 & SB 727-55A0091. INSTALLED NEW RIB WITH P/N 65-17428-6 IAW SRM 51-30-2 & SB 727-55A0091.SDR 04FDEA03450Structure · crackedN01259 RT HAND HORIZONTAL STAB L/E UPPER CHORD CRACKED ON LWR SURFACE BETWEEN L/E STAB STA 1.0 TO L/E STAB STA 72.0. FOUND RT HORIZ STAB L/E UPR CHORD OUT OF LIMITS. TRIMMED OUT SEGMENT OF CHORD, FABRICATED NEW CHORD FROM REF. PO 179160, SPLICE FROM BAC1490SDR 04FDEA03437Frame · corrodedFLT CREW COMPARTMENT LEFT SIDE AT FS 227.8 FRAME HAS 2 EACH AREAS OF CORROSION ABOVE AND BELOW OXYGEN PANEL. REMOVED DAMAGE AREA IAW SRM 51-40-2, MADE NEW WEB FROM 7075-T6 .125C BATCH 0000828965 & DOUBLER MADE FROM 7075-T6 .160C BATCH 0000687676 IAW SRM 51SDR 04FDEA03436Skin · crackedEXTERNAL SKIN CRACKED AT AFT LWR CARGO DOOR CUTOUT 10 INCHES AFT OF THE FWD LWR CORNER 2 INCHES BELOW LWR EDGE. REPAIRED CRACKED SKIN, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA 7-5330-82517.SDR 04FDEA03433Web · chafedLT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BSDR 04FDEA03432Web · chafedLT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BSDR 04FDEA03411Spar · crackedWHILE ACCESSING FRONT SPAR WEB FOR UPR SPAR REPAIR, LWR FRONT SPAR VERTICAL FLANGE CRACKED BETWEEN LT L/E STA 109 & 119. REPAIRED IAW SRM 55-10-5.SDR 04FDEA03404Web · corrodedCORROSION LT HORIZONTAL STAB FIXED L/E INTERNAL VERTICAL WEB L/E STA 29. *S/D* REPAIRED PER SRM 55-10-1 FIG 1, 51-30-2, 51-10-1, 55-10-4, 51-30-5.SDR 04FDEA03401Skin · damagedCOMPLY WITH EO 7-5330-7-2319 PART 5 BS 441 AT STR 19-20 RT AND STR 20-21 RT. *S/D* REPAIRED FUSE SKIN BS 441 STR 19-21 RT IAW EO 7-5330-7-2319 AND EA 7-5330-82513.SDR 04FDEA03181Skin · gougedUPPER EXTERNAL SKIN BS 761, 2 INCHES ABOVE STR 4 LT IS GOUGED. BLENDED GOUGE ON SKIN BS 761, 2 INCHES ABOVE STR 4 LT, OUT OF LIMITS. REPAIRED DAMAGE SKIN AT BS 761 STR 4 LT PER SRM 53-30-3 FIG 5.SDR 04FDEA03164Skin · corrodedCORROSION BS 480 STR 4R - STR 6R UNDER FWD SIDE OF THE SPLICE. FOUND VISUALLY, DURING DETAILED VISUAL INSPECTION. CORROSION NOT FOUND DURING LOW FREQUENCY INSPECTION. CORROSION BS 480 STR 4R TO 6R UNDER FWD SIDE OF SPLICE REPAIR ON W/C N01202 AND EO 7-533SDR 04FDEA03165Hinge · corrodedCORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE.SDR 04FDEA03163Attach Fitting · damagedLT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING.SDR 04FDEA03076Spar · crackedN01167 CORROSION ON LT. HORIZ. STAB UPPER SPAR AT STAB STA. 198. REPAIRED PER SRM 55-10-5 FIG 1SDR 04FDEA03032Frame · dentedAFT CARGO FRAME DENTED AT BS. 1010 STR 26R. REPAIRED PER SRM 51-40-3SDR 04FDEA03039Stringer Clip · crackedSTRINGER CLIP CRACKED BS 1108 LT STR 20. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 04FDEA03038Door Frame · damagedBS 1108 AFT CARGO DOOR FRAME AT STR 26 HAS A OPEN HOLE IN UPPER FLANGE. REPAIRED AFT CARGO DOOR FRAME PER FED EX EA 7-5310-825111.SDR 04FDEA03037Stringer · gougedGOUGE ON UNDERSIDE FLANGE OF STR 19 RT, BS 488, WL 174. REPAIRED STR 19 RT IAW SRM 53-10-3 FIG 1 AND 53-10-1.SDR 04FDEA03036Frame · dentedFWD CARGO STA 540 FRAME DENTED AT STR 24 LT & 25 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-1, 51-20-4, 53-10-1.SDR 04FDEA03035Frame · dentedFWD CARGO FRAME STA 660 DENTED STR 24 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-4 AND 53-10-1.SDR 04FDEA03034Frame · dentedTOP FLANGE OF FRAME AT BS 640, RBL 32, WL 150 IS DENTED. REPAIRED PER SRM 53-10-1, 51-30-5, 51-20-4, 51-30-2, 51-10-1, 53-10-2 AND 51-40-3SDR 04FDEA03033Rib · crackedRT ELEVATOR NR 5 HINGE SUPPORT RIB ELEVATOR STA 136.50 PREVIOUS REPAIR AT I/B LOWER FLANGE IS CRACKED. REPLACED PER E.O. 7-5510-7-5001 PT 2.SDR 04FDEA03031Frame · dentedFRAME DENTED AT BS 1090, STR 23 LT. REPAIRED PER SRM 51-40-3.SDR 04FDEA03030Frame · dentedAFT CARGO FRAME DENTED AT BS 990, STR 26R. REPAIRED PER SRM 51-40-3.SDR 04FDEA03023Fire Warning · false activationENGINE FIRE INDICATION NR 2 ENGINE. RAN RED TABS, SHUT DOWN ENGINE, DID NOT FIRE BOTTLES. INDICATION EXTINGUISHED AFTER 10 SEC, BEFORE POWER LEVER WAS MOVED TO IDLE, INDICATION OCCURED DURING CLIMB ABOUT 7,000 FT, 90 PERCENT N1, EPR 1.85. ALSO ENGINE WAS WSDR 04FDEA02959Engine · overtempPDIS 192 79-10 0009533 20OCT04 MEM OPEN U LOGPAGES: 00949069 ENG NR 2 AND NR 3 OIL TEMPS BOTH IN THE YELLOW BAND AND OCCASSIONALLY SPIKING INTO THE RED DURING CLIMBOUT BOTH ENGINE HAD TO BE KEPT ABOVE IDLE TO MAINTAIN LOWER TEMPS.SDR 0041005Wire · shortedAFTER TAKEOFF AT 1000 FT, A BURNING ODOR NOTED, NO OBVIOUS PROBLEM WITH GEN LOADS, APPROX 3000 FT VISIBLE SMOKE EMINATING BEHIND FE TABLE. NO CB'S POPPED, NO VISIBLE SYS TROUBLE. TROUBLE CEASED & SMOKE CLEARED. ENGINEER DETERMINED ALL SYSTEMS OPERATIONAL. AS ISDR 04FDEA02265Skin · corrodedCORROSION ON INNER SKIN AT AFT CARGO DOOR AFT CUTOUT LOWER CORNER. REPAIRED INNER SKIN AT AFT CARGO DOOR AFT CUT OUT LOWER CORNER PER FED EX E.A. 7-5310-55341.SDR 04FDEA02264Door Frame · corrodedCORROSION AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD CONTINUING UNDER FILLER. REPAIRED AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD PER FED EX E.A. 7-5310- 55341.SDR 04FDEA02263Stringer · corrodedCORROSION ON UPPER SURFACE OF STRINGER 7L STA 876. CORROSION DAMAGE ON UPPER SURFACE OF STRINGER 7L, STA 876 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED DAMAGED STRINGER SECTION BS 870 - 890+10, STR 7L PER SRM 51-10-5 AND 51-30-2. FASDR 04FDEA02266Skin · crackedCRACK IN SKIN AT EDGE OF LAP JOINT BS 1064 RBL 26 STR 26R.SDR 04FDEA02180Skin · dentedDENT IN FUSELAGE SKIN BS 320-330 AND 2 INCHES ABOVE STR 21R. REPAIRED THE FUSELAGE SKIN AT BS 320 TO 330 2 INCHES ABOVE STR 21R PER EA 7-5330- 70671SDR 04FDEA02191Stringer · crackedWHILE WORKING CARD N00533, FOUND CRACKED STRINGER AT BS 1114 STR 25 RT. *S/D* REPAIRED STRINGER 25 RT AT BS 1107-1115 PER SRM 53-10-3 FIG 1.SDR 04FDEA02190Seat Track · corrodedCORROSION AROUND SEAT TRACK LINK AFT ATTACH BOLT BS 870 LBL 25 WL 205. *S/D* CORROSION ON AROUND SEAT TRACK LINK ATTACH BOLT AT BS 870 LBL 25 WL 205 WAS FOUND TO BE IN LIMITS. CORROSION ON LINK AT BS 870 LBL 25 WL 208 WAS OUT OF LIMITS. REMOVED & REPLACED SDR 04FDEA02189Seat Track · corrodedCORROSION SEAT TRACK BS 870-950, RBL 45, WL 208. CORROSION ON SEAT TRACK AT BS 870-950 RBL 45 WL 208 WAS FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-5.SDR 04FDEA02188Seat Track · corrodedCORROSION SEAT TRACK BS 760-840 RBL 22 WL 208. REMOVED AND REPLACED LONGITUDAL BEAM STA 760-848 RBL 22, WL 208 IAW SRM 51-30-02, 51-30-5.SDR 04FDEA02187Seat Track · corrodedCORROSION SEAT TRACK BS 760-840 LBL 25 WL 208 AT FASTENER HOLES. REMOVED CORROSION ON SEAT TRACK FROM BS 760-840 LBL 25 WL 208 FOUND SEAT TRACK TO BE OUT OF LIMITS. LOCATED AND DRILLED HOLES ON NEW LONGITUDAL BEAM AND INSTALLED IAW SRM 51-30-2.SDR 04FDEA02186Seat Track · damagedCORROSION SEAT TRACK BS 870, LBL 45, WL 208. REMOVED CORROSION ON SEAT TRACK STA 870 LBL 45, WL 208. REMOVED .040, 1 INCH X 1 INCH FROM .080. OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED, ALODINED AND PRIMED NEW SEAT TRACK, INSTALLED NEW SEASDR 04FDEA02185Angle · dentedFWD CARGO COMPARTMENT J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. *S/D* FOUND J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. REMOVED, FABRICATED AND INSTALLED NEW J-ANGLE IAW SRM 53-10-1 PG 2 FIG 1 SHEET 2, SRM 51-30-2.SDR 04FDEA02184Seat Track · corrodedCORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 RBL 48 WL 205. *S/D* CORROSION ON LINK AT BS 742 WAS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK LINK AND FWD ATTACH BOLT AT BS 742 RBL 48 WL 205 PER SRM 51-30-2, 53-10-1 & 53-10-5 & AT BS 740-760 R
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