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 96FDEA01165Shear Tie · corrodedNR0516 AND 047, CORROSION (C53-111-01-3), (C53-113-01-2) ON FRAME SHEAR TIE AT BS 970 LBL 12 WL 139. *S/D* BLENDED CORROSION ON SHEAR TIE, FOUND TO BE OUT OF LIMITS. REPAIRED PER FEDEX SRM 53-10-4.Jun 21, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01160Floor Beam · elongated holeNR0669 AND 046, WHILE WORKING NR0553 SEAT TRACK DISCOVERED 740 FLOOR BEAM TO HAVE ELONGATED HOLE AT WL 208 LBL 25. *S/D* REAMED HOLE ON FLOOR BEAM AT BS 740 LBL 25 TO A SIZE OF .4195. INSTALLED FREEZE PLUG WITH SEALANT AND INSTALLED PERMANENT STRAP IAW FEDEJun 20, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01147Floor Beam · corrodedNR0485 AND 045, CORROSION ON FLOOR BEAM BS 1110 AROUND NUTCLIP HOLES WL 208 RBL 25 TO 54. *S/D* REMOVED CORROSION AND REPAIRED TOP CHORD OF FLOOR BEAM BS 1110 WL 208 RBL 10 TO 65 PER FEDEX SRM 53-10-8.Jun 19, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01146Floor Beam · corrodedNR0440 AND 044, CORROSION (C53-111-01) ON LOWER FLOOR BEAM FLANGE AT BS 1130 RBL 29, 36 LBL 8 AND 20 WL 200. *S/D* REMOVED CORROSION FROM LOWER FLOOR BEAM FLANGE AT BS 1130 RBL 29, 36 LBL 8 AND 20 WL 200. REPAIRED IAW FEDEX SRM 53-10-08 FIG 8 AND EX EA 7-53Jun 16, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96DHL708005Cdi · failedCAPT'S NR 1 VOR CDI IS STUCK IN THE CENTER. REMOVED AND REPLACED NR 1 CDI.Jun 14, 1996 · N708DH · Boeing 72725 · Integrated Flight SystemSDR 96FDEA01091Beam · corrodedNR0664 AND 042, CORROSION ON BEAM AT WL 235 RBL 15.5 TO 18.5 LOWER SIDE BS 1336 TO 1342.Jun 11, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR CA960619001Oil Pressure · low(CAN) #1 ENGINE OIL PRESSURE LOW ON TAKEOFF, ABORTED. NO FAULT FOUND.Jun 3, 1996 · Boeing 72725 · Engine Oil Indicating SystemSDR 96FDEA01058Skin · corrodedCORROSION (C53-224-04) ON INSIDE OF SKIN EMANATING FROM WINDOW FRAME AT BS 1094, 4 INCHES ABOVE STR 11L. REMOVED CORROSION FROM WINDOW DOUBLER, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION FROM SKIN AND FRAME FOUND TUBE WITHIN LIMITS. REPAIRED WINDOW FRAME May 31, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA01057Skin · corrodedCORROSION (C53-224-04) ON INSIDE SKIN EMANATING FROM WINDOW FRAME AT BS 1083 TO 1086 STR 11L. REMOVED CORROSION FROM WINDOW DOUBLER FOUND TO BE OUT OF LIMITS. THE SKIN AND FRAME WERE FOUND TO BE IN LIMITS. REPAIRED DOUBLER PER EA 7-5330-28369.May 31, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA1041Splice Angle · corrosionWHILE WORKING NR0488, FOUND CORROSION ON SPLICE ANGLE AFT SIDE BS 870 TERMINAL FITTING, STR 9L. REMOVED SPLICE ANGLE ON AFT SIDE OF BS 870 TERMINAL FITTING STR 9L AND REPLACED PER FEDEX SRM 51-10-1.May 29, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01040Angle · corrosionWHILE WORKING ON NR0488, FOUND CORROSION ON SPLICE ANGLE AT BS 870 TERMINAL FITTING STR 9L FWD SIDE. REMOVED SPLICE ANGLE ON FWD SIDE OF 870 TERMINAL FITTING, STR 9L AND REPLACED PER FEDEX SRM 51-10-1.May 29, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR CA960605002Strut · leaking(CAN) WHEN GEAR WAS SELECTED UP ON CLIMB OUT THE NOSE GEAR DOOR LIGHT REMAINED ON AND THERE WAS AN UNSAFE LANDING GEAR WARNING, GEAR EXTENDED AND AIRCRAFT LANDED.May 24, 1996 · Boeing 72725 · Nose/Tail Landing Gear Strut/AxleSDR 96FDEA1015Air Distr · odorSTRONG ACRID ODOR IN COCKPIT AT FLIGHT LEVEL 330. PACK TEMPERATURES NORMAL, NOTHING ABNORMAL INDICATED AND DETECTION SYSTEM TESTED NORMAL. SUSPECT EITHER ELECTRICAL MALFUNCTION OR TOILET CHEMICAL MIXING CAUSED TOXIC FUMES. NO VISIBLE SMOKE. AIRCRAFT RELEASMay 22, 1996 · N154FE · Boeing 72725 · Air Distribution SystemSDR 96FDEA01009Skin · corrodedWHILE WORKING NR 0351, FOUND CORROSION IN SKIN LAP BETWEEN BONDED DOUBLER AND LOWER SKIN AT BS 1080 - BS 1110, STR 14L. CUT OUT TO REMOVE CORROSION AND REPAIRED SKIN LAP AT BS 1080 - BS 1110, STR 14L PER FEDEX SRM 53-30-3.May 20, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA01008Stringer · corrodedCORROSION ON STR 1, BS 414 - BS 420. COMPLETED REPAIR ON STR 1, BS 414 - BS 420, PER FEDEX SRM 53-10-3.May 20, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00992Beam · corrodedCORROSION ON BEAM AT RBL 18 TO 75 WL 205 BS 1344 TO 1379. REMOVED AND REPLACED BEAM AT BS 1344 TO 1379 WL 255 RBL 255.May 17, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00991Blkhd Stiffener · corrodedS-DUCT OPENING CIRCUMFERENTIAL STRAP AND STIFFENER ON 1342 BULKHEAD RT SIDE, WL 180 - WL 270, RBL 15.5 IS CORRODED. REMOVED AND REPLACED CIRCUMFERENTIAL STRAP AND STIFFENER ON BS 1342, RBL 15.5, WL 180 - WL 270. (STIFFENER P/N 69154056).May 17, 1996 · N506FE · Boeing 72725 · Fuselage Main, BulkheadSDR 96FDEA00990Bracket · corrodedCORROSION C53-10-01(1) AROUND UPPER FASTENERS ON FORGING BS 228, LBL 6 - LBL 13, WL 184. REMOVED AND REPLACED FORGING BRACKET AT BS 228, LBL 6 - LBL 13, WL 184.May 17, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00989Skin · damagedCORROSION C53-100-01 SKIN AND DOUBLER BULGING BS 334 - BS 352, LBL 21 - LBL 26, WL 145. REMOVED FASTENERS FROM SKIN, FOUND NO CORROSION UNDER SKIN OR DOUBLER. FABRICATED DOUBLER AND INSTALLED, AND INSTALLED ALL FASTENERS IAW SRM 53-30-03.May 17, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00985Stringer · corrodedCORROSION (C53-224-04) ON STR 3L AT BS 950 TO 985. REMOVED CORRODED SECTION OF STR, FABRICATED AND INSTALLED REPAIR AT BS 950 TO 985 STR 3L IAW SRM 53-10-3.May 16, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00984Floor Beam · corrodedCORROSION BS 312 FLOOR BEAM WL 208 LBL 4 TO 19 AND 30. CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW BEAM AND REPAIR PARTS AND INSTALLED BS 312 LBL 65 TO RBL 8 WL 208 IAW FEDEX SRM 53-10-8.May 16, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00983Seat Track · corrosionSEAT TRACK RBL 45 CORROSION ON SPLICE AT BS 950 PLUS 10 WL 208. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK BS 950 PLUS 10 TO 870 RBL 45 PER FEDEX SRM 53-10-5.May 15, 1996 · N505FE · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00970Skin · delaminatedNR0402 AND 022, RT ELEVATOR TAB T/E O/B CORNER IS DELAMINATED. *S/D* REPAIRED RT ELEVATOR TAB IAW FEDEX SRM 51-40-06 AND 51-80-09.May 13, 1996 · N505FE · Boeing 72725 · Horizontal Stabilizer, Tab StructureSDR 96FDEA00969Chord · corrosionNR0316 AND 024, CORROSION (C53-224-05) ON THE BS 740 LWR CHORD RBL 15 TO 20 ON VERTICAL FLANGE. *S/D* REMOVED LOWER CHORD, CORROSION WAS OUT OF LIMITS, LOCATED NEW LOWER CHORD, DRILLED, FABRICATED SPLICES, TREATED AND INSTALLED ALL PARTS IAW FEDEX EA 7-5710-May 13, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00967Support · corrodedCORROSION (C53-100-01) ON TOP AND BOTTOM FLANGES OF FAIRING SUPPORT CHORD BS 351 LBL TO RBL 17 WL 145 AT VARIOUS LOCATIONS. REMOVED FAIRING SUPPORT CHORD BS 351 LBL TO RBL 17 WL 145 AND REPLACED WITH NEW CHORD PER FEDEX SRM 51-30-2.May 13, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00966Stringer · crackedCRACK IN THE HORIZONTAL FLANGE OF STR 17R AND BS 849. CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER ANGLES, RADIUS FILLERS, DRILLED UP REPAIR PARTS, ALODINED AND PRIMED AND INSTALLED WET WITH SEAL PER FEDEX SRM 51-40-4.May 13, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00947Floor Beam · corrodedCORROSION BS 360 FLOOR BEAM WL 208 RBL 5. CUT OUT DAMAGED PORTION OF FLOOR BEAM AT BS 360 WL 208 RBL 6 TO LBL 10 AND REPAIRED PER FEDEX SRM 53-10-8.May 10, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR CA960524015Oil System · oil leak(CAN)ON CLIMBOUT, #2 ENGINE OIL PRESSURE DROPPING, ENGINE SHUTDOWN INTERNAL OIL LEAK TOWARD THE AFT OF ENGINE. FOLLOW-UP COMINGMay 9, 1996 · Boeing 72725 · Turbine Engine Oil SystemSDR 96FDEA00930Floor Beam · corrodedCORROSION (C53-224-01, -1) ON UPPER FLANGE OF FLOOR BEAM BS 680 BETWEEN LBL 9 TO 13 LBL 19 TO 2 RBL 10 WL 208. REMOVED CORRODED UPPER FLANGE OF FLOOR BEAM BS 680 LBL 31.5 TO RBL 12 WL 208. FABRICATED, CLEANED, TREATED AND INSTALLED REPAIR PARTS IAW FEDEX SRMMay 9, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00929Frame · corrodedCORROSION (C53-111-01, -2) IN FWD CARGO BAY ON FRAME AT BS 680 RBL 62 WL 196. REMOVED CORRODED AREA OF FRAME AT BS 680 RBL 62 WL 196 AND REPAIRED IAW FEDEX SRM 51-40-3.May 9, 1996 · N505FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00926Stringer Tie · damagedMECHANICAL DAMAGE ON STR EXTENSION ON BOTH SIDES OF THE BS 950 FORGING AT STR 8L. REMOVED AND REPLACED STR EXTENSION ON BOTH SIDES OF THE BS 950 FORGING AT STR 8L.May 8, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00925Floor Panel · corrosionNR0420 AND 016, CORROSION (C53-221-01) ON FLOOR PANEL UNDER WIRE BUNDLE ON RT SIDE OF CENTER CONSOLE BS 200 TO 288 WL 208 RBL 4 TO 12.May 8, 1996 · N505FE · Boeing 72725 · Fuselage Floor PanelSDR 96FDEA01016Tear Strap · corrosionNR0564 -032C, WHILE WORKING NRO498 DISCOVERED CORROSION IN BETWEEN BONDED DOUBLER AND OVERLAPPED SKIN BS 418 TO 464 STR 4R. ACCESSED REPAIR AREA, FOUND BONBED TEAR STRAP CORRODED BEYOND LIMITS. REMOVED FABRICATED AND INSTALLED BONDED TEAR STRAP, REINSTALLED May 7, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00921Stringer · crackedNR0099 AND 011, STR 20R CRACKED AT EQUIPMENT COOLING DUCT CLAMP AREA AT STA 359.May 7, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00920Skin · corrodedNR0496 AND 013, CORROSION BETWEEN SKIN AND BONDED DOUBLER AT BS 360 STR 5 TO 6R.May 7, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00919Skin · corrodedNR0498 AND 014, BOND DEGREGATION IN THE FORM OF CORROSION AT BS 441 BETWEEN STR 14 TO 15R, 3.5 BY .3 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGE SECTION AT BS 441 RT, FABRICATED REPAIR PARTS AND INSTALLED AND SEALED PER FEDEX EO 753330-May 7, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00917Support · corrodedNR0415 AND 036, CORROSION UNDER NUTPLATES ON FRAME UNDER FLOOR SUPPORT.May 7, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00916Floor Beam · corrosionCORROSION (C53-111-01) ON LOWER FLANGE OF FLOOR BEAM BS 540 LBL 12 WL 200. REMOVED DAMAGED AREA OF BEAM AT BS 540 WL 200 RBL 28 TO LBL 20 AND INSTALLED REPAIR PART PER FEDEX SRM 53-10-5 FIG 2.May 7, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00910Skin · corrodedNR0659 AND 035, CORROSION ON INNER SKIN STA 308 LBL 49 WL 180. *S/D* REPAIRED CORROSION ON INNER SKIN STA 308 LBL 49 WL 180 PER FEDEX SRM 53-30-03.May 6, 1996 · N506FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00909Door Frame · corrodedNR 0057 AND 034. CORROSION UNDER LATCH SERRATED PLATE OF FORWARD CARGO DOORWAY AFT FRAME. **********S/D ********** COMING.May 6, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00908Floor Beam · corrosionNR 0439 AND NR 033. CORROSION ON LOWER FLOOR BEAM FLANGE AT BS 1148, RBL 14, 27, 36 AND LBL 8 AND 21, WL 200. *****S/D***** REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM PER FEDEX SRM 53-10-8.May 6, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00907Beam · crackedFORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED IN LOWER FORWARD STOP PIN FITTING. REPAIRED FORWARD ENTRY DOOR LOWER GATE BEAM IAW FEDEX EA 7-5210-28328.May 6, 1996 · N505FE · Boeing 72725 · Passenger/Crew DoorsSDR 96FDEA00906Skin · damagedEXTERNAL SKIN HOLE IN SKIN BS 1178 AT STR 22L. REMOVED DAMAGED SKIN AT BS 1178, STR 22L AND INSTALLED REPAIR DOUBLER AND FILLER. ALL WORK DONE PER FEDEX SRM 53-30-3.May 6, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00895Stringer · corrodedCORROSION ON STR 1 BS 414 TO 420. *S/D* COMPLETED REPAIR ON STR 1 BS 414 TO 420 PER FED EX SRM 53-10-3.May 6, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA01089Web · crackedWHILE WORKING NR0316, FOUND HOLE TO BE CRACKED UNDER STIFFENER AT BS 740 WEB LBL 55 WL 185. REMOVED BS 740 WEB AND INSTALLED NEW BS 740 WEB PER FEDEX DRAWING 64-18333 AND EA 7-5710-28401.May 4, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00903Floor Beam · corrosionNR0533 AND 009, CORROSION (C53-224-01, -1) ON UPPER FLANGE FLOOR BEAM PREVIOUS REPAIR BS 620 BETWEEN LBL 22 TO RBL 11 WL 208. *S/D* REMOVED CORRODED UPPER FLANGE FLOORBOARD PREVIOUS REPAIR BS 620 BETWEEN LBL 22 TO RBL 11, WL 208. FABRICATED NEW CHORD AND REMay 4, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00902Floor Beam · corrodedNR0469 AND 008, CORROSION AT BS 344 FLOOR BEAM LBL 40 TO RBL 15 WL 208. ACCOMPLISHED FLOOR BEAM REPAIR AT BS 344 LBL 40 TO RBL 15 WL 208 PER FED EX DRW SR 27-53-007.May 4, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00897Act Bracket · crackedNR 0089 AND NR 002, NR 2 K-FLAP ACTUATOR AFT I/B MOUNT IS CRACKED AT UPPER FWD CORNER. ****S/D ****** COMING. REMOVED AND REPLACED NR 2 K-FLAP ACTUATOR APT I/B MOUNT IAW FEDEX SRM 51-10-1 AND 51-30-2.May 3, 1996 · N505FE · Boeing 72725 · Leading Edge Slat ActuatorSDR 96FDEA00896Floor Beam · corrodedNR 0514 AND 003, CORROSION C53-224-01(1) ON UPPER FLANGE OF FLOOR BEAM BS 640 BETWEEN RBL 14 - 43, WL 208. *****S/D***** COMING.May 3, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00894Skin · damagedNR0438 AND 005, EXTERNAL SKIN HOLE IN SKIN BS 1178 AT STR 22L. *S/D* REMOVED DAMAGED SKIN AT BS 1178 STR 22L AND INSTALLED REPAIR DOUBLER AND FILLER. ALL WORK DONE PER FEDEX SRM 53-30-3.May 3, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
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