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 96FDEA00893Floor Beam · corrodedNR0481 AND 006, CORROSION (C53-224-01) ON BS 560 FLOOR BEAM AT LBL 36 TO 7, RBL 8 WL 208. *S/D* REMOVED CORRODED FLOOR BEAM UPPER FLANGE AT LBL 43.5, RBL 13.5 WL 208. FABRICATED REPAIR PARTS, CLEANED AND TREATED, FASTENED INTO PLACE IAW FEDEX SRM 53-10-8.May 3, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00891Bullnose · corrodedCORROSION ON NR 5 K-FLAP AT 1/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT. REPAIRED AREA PER FEDEX SRM 57-50-3.May 3, 1996 · N506FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00890Uplock Switch · malfunctionedRT MAIN GEAR DOOR LIGHT WOULD NOT GO OUT AFTER RAISING GEAR, LIGHT STAYED ON AFTER LANDING GEAR RECYCLED FOR LANDING. *S/D* REPLACED RT MLG DOOR UPLOCK SWITCH PER MM 32-62-11, OPS CKS NORMAL.May 2, 1996 · N152FE · Boeing 72725 · Landing Gear Position and WarningSDR 96FDEA00889Stringer · corrodedNR 0547 AND NR 029, CORROSION UNDER STANDOFF ON STR 28L AT BS 408. ******S/D****** COMING.May 2, 1996 · N506FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00888Floor Beam · damagedDAMAGED FLOOR BEAM (LOWER) DUE TO SCREW PROTRUSION CHAFING AT BS 680, LBL-RBL 18 (11 PLACES) WL 200. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, DRILLED, AND INSTALLED. WORKED IAW FEDEX SRM 53-10-8, FIG 2.May 2, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00886Bulkhead Fitting · crackedNR0089 AND 027, CRACK IN FLANGE OF 740 FORGING RT SIDE FROM STR 19R TO INTERCOSTAL. *S/D* REPLACED 740 FORGING RT SIDE PER FEDEX EA 7-5310-29171.May 2, 1996 · N506FE · Boeing 72725 · Fuselage Main, BulkheadSDR 96FDEA00881Skin · disbondedRIGHT WING INBOARD FOREFLAP INBOARD RUB STRIP MISSING. UPON FURTHER INVESTIGATION, FOUND A 7.50 INCH BY 3.25 INCH PREVIOUS REPAIR IN RUB STRIP AREA TO BE DISBONDED. ******S/D****** REPAIRED DAMAGED SKIN TO RIGHT WING INBOARD FOREFLAP RUB STRIP AREA IAW FEDMay 2, 1996 · N506FE · Boeing 72725 · Trailing Edge FlapsSDR 96FDEA01088Fitting · crackedON INSPECTION OF BS 870 TERMINAL FITTING LT ROW, 2 NOTED CRACK INDICATIONS IN 2ND AND 3RD HOLE FROM TOP. REMOVED EXISTING REPAIR, REMOVED EXISTING FASTENERS IN REPAIR AREA, STOP DRILLED CRACK, BLENDED CORROSION, FABRICATED REPAIR PARTS, TREATED MATERIAL, INSTMay 1, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01087Skin · corrodedBOND DEGRADATION IN THE FORM OF CORROSION AT BS 441 STR 15 AND 16L, .4 BY 8 AREA MARKED. ALSO, BETWEEN STR 17 AND 18L, .3 BY 2 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED SECTION OF SKIN AND REPAIRED PER FEDEX EA 7-5330-29115 EA 7-531May 1, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00880Floor Beam · corrodedNR0555 AND 024, CORROSION AT BS 620 FLOOR BEAM WL 208 LBL 17 TO 51. *S/D* REPAIRED FLOOR BEAM BS 620 WL 208 RBL 15 TO LBL 51 PER FEDEX SRM 53-10-8.May 1, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01086Frame · crackedSTA 783.95 RBL 65 WL 202 WHILE WORKING CARD 7-5310-7-33678 PT 4, FOUND A CRACK ON INSIDE FRAME WEB, STARTING FROM FASTENER HOLE, BOTTOM AFT SIDE OF FRAME. REMOVED EXISTING FASTENERS FABRICATED REPAIR PARTS DRILLED AND TREATED MATERIAL PLUGGED REQUIRED FASTENEApr 30, 1996 · N505FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00873Shear Tie · corrodedNR0520 AND 019, CORROSION ON FRAME SHEAR TIE AT BS 1050 LBL 10 WL 141. *S/D* BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PART AS PER FEDEX SRM 53-10-4 FIG 11.Apr 30, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00872Bullnose · corrosionNR0154 AND 018, DUE TO NUMEROUS AREAS OF CORROSION NR 5 BULLNOSE REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 5 K-FLAP BULLNOSE IAW FEDEX OHM 57-51-11, MM 27-81-1, AND MM 27-81-11.Apr 30, 1996 · N506FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00871Flap · corrosionNR0153 AND 017, DUE TO NUMEROUS AREAS OF CORROSION NR 1 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED NR 1 K-FLAP AND SENT OUT FOR REPAIR. RECEIVED SERVICEABLE REPAIRED NR 1 K-FLAP AND INSTALLED IAW FEDEX MM 27-81-1 AND MM 27-81-11.Apr 30, 1996 · N506FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00870Flap · corrodedNR0152 AND 016, DUE TO NUMEROUS AREAS OF CORROSION NR 2 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 2 K-FLAP IAW FEDEX MM 27-81-1 AND MM 27-81-11.Apr 30, 1996 · N506FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00869Flap · corrosionNR0151 AND 015, DUE TO NUMEROUS AREAS OF CORROSION NR 3 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 3 K-FLAP IAW FED EX MM 27-81-1 AND MM 27-81-11.Apr 30, 1996 · N506FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00868Flap · corrosionNR0150, 014, DUE TO NUMEROUS AREAS OF CORROSION NR 4 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 4 K-FLAP IAW FED-EX MM 27-81-1, FUNCTIONAL TEST GOOD IAW MM 27-81-1.Apr 30, 1996 · N506FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA00860Skin · gougedNR0591 AND 013, GOUGE IN SKIN AT BS 1344 LBL 29 WL 155. *S/D* CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED AT BS 1344 LBL 29 WL 185 AS PER SRM 54-30-3.Apr 26, 1996 · N506FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00859Skin · crackedNR0590 AND 012, CRACK SKIN AT BS 1352 RBL 23 WL 192. *S/D* REMOVED DAMAGE AREAS AT BS 1352 RBL 23 WL 192.195, FOUND TO BE IN LIMITS PER FEDEX EA 7-5330-28356.Apr 26, 1996 · N506FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00857Shear Tie · corrosionNR0521 AND 010 CORROSION ON FRAME SHEAR TIE AT BS 1030 RBL 10 WL 141.Apr 26, 1996 · N506FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00858Skin · gougedNR0583 AND 011, 3 GOUGES IN SKIN AT BS 1229 RBL 41 WL 180.Apr 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00856Frame · crackedFRAME CRACKED AROUND FASTENER HOLE BS 990 I/B OF STR 4R. REPAIRED CRACK AT BS 990 I/B OF STR 4R AT FASTENER HOLE. ALODINED AND PRIMED, DONE IAW FEDEX SRM 53-10-4.Apr 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00850Extend Switch · malfunctionedDURING FLAP RETRACTION THE NR 7 SLAT FAILED TO RETRACT. AMBER LIGHT REMAINED ON AT PILOT'S PANEL AND GREEN LIGHT REMAINED ON AT THE SLAT/FLAP INDICATOR PANEL. REPLACED NR 7 SLAT ACTUATOR, DID NOT CURE PROBLEM IAW 727-100 MM PAGE 401 TO 409 CHAP 27-81-32. REApr 25, 1996 · N510FE · Boeing 72725 · Leading Edge Slat Control SystemSDR 96FDEA00849Bolt · missingAFTER T/O, NR 3 ENG THROTTLE DID NOT AFFECT ENGINE PRODUCTION, APPEARS AS IF THROTTLE LINKAGE DISCONNECTED. SHUT ENGINE DOWN USING NORMAL PROCEDURES. FOUND A BOLT HAD FALLEN OUT OF LINKAGE ON NR 3 ENGINE. REINSTALLED COTTER PIN AND CHECKED RIG WHICH WAS GOOApr 25, 1996 · N154FE · Boeing 72725 · Power LeverSDR 96FDEA00846Frame · corrodedNR0386 AND 004, CORROSION ON FRAME BS 148 BETWEEN STR 14 TO 15R. *S/D* REMOVED DAMAGED FRAME DOUBLER AND FAIL-SAFE, REPLACED WITH FABRICATED REPAIR PARTS AT BS 1130 BETWEEN STR 14R AND 15R IAW FEDEX SRM 51-40-3 FIG 1 53-10-2.Apr 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00845Frame · crackedNR0396 AND 005, CRACKED FRAME AT BS 580 WL 154 RBL 18 UNDER FLOOR SUPPORT. *S/D* REMOVED DAMAGED AT BS 580, WL 154, RBL 18, FABRICATED REPAIR DOUBLER AND INSTALLED IAW FEDEX SRM 51-40-3 UNDER FLOOR SUPPORT.Apr 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00843Floor Beam · chafedNR0400 AND 007, DAMAGED LOWER FLOOR BEAM DUE TO SCREW PROTRUSION CHAFING AT BS 680 LBL TO RBL 18 WL 200. *S/D* REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, DRILLED AND INSTALLED WORKED IAW FEDEX SRM 53-10-8 FIG 2.Apr 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00842Skin · delaminatedNR0435 AND 008, SKIN INTERNAL BONDED DOUBLER IS DELAMINATED AT BS 1148 TO 1166 BETWEEN STR 23 TO 25R. *S/D* REPAIRED PER FEDEX EA 7-5330-28332.Apr 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00927Floor Beam · corrodedCORROSION (C53-111-01) ON LOWER FLOOR BEAM FLANGE BS 1030 RBL 47 WL 200. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 4. REPAIRED LOWER FLOOR BEAM FLANGE AT BS 1030 RBL 47 WL 200 IAW SRM 53-10-8 FIG 8.Apr 24, 1996 · N506FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96DHL708004Ballast · failedSMOKE IN COCKPIT, ISOLATED TO GLARE SHEILD FLOOD LIGHT BALLAST M356 AND M357. PULLED AND COLLARD C/B.Apr 20, 1996 · N708DH · Boeing 72725 · Flight Compartment LightingSDR 96FDEA00785Beam · corrodedWHILE WORKING NR0470, FOUND CORROSION ON 740 BEAM UPPER SEAT AT LBL 25.Apr 15, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00784Skin · corrodedCORROSION BETWEEN SKIN AND WINDOW CUTOUT DOUBLER BETWEEN STR 10 TO 11R STA 1083. REMOVED WINDOW FRAME, FOUND CORROSION TO BE OUT OF LIMITS ON FRAME AT 2 AREAS OF OUTER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLES ON OUTER SKIN AND REPLACED FRAME IAW FEDEX EApr 15, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00783Chord · crackedCRACK IN REINFORCEMENT CHORD ON UPPER FUEL CELL SKIN BS 745 WL 204.5 RBL 45.5. REMOVED DAMAGED CHORD BS 745 TO 783 RBL 45 WL 204. FABRICATED NEW CHORD AND INSTALLED IAW FEDEX EA 7-5710-28237.Apr 15, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00762Skin · corrodedEXTERIOR SKIN SURFACE IS BULGING AND HAS TWO SKIN PLUGS MISDRILLED AT BS 330 - 334 AT LOWER LT NOSE CHORD STR 27L. REMOVED SKIN IN AREA OF REPAIR PLUGGED HOLES AND FABRICATED REPAIR FILLER AND DOUBLER. INSTALLED REPAIR PARTS PER FEDEX EA 7-5330-28230.Apr 12, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR DHL96708002Aileron Spring · wornLEFT CONTROL YOKE INPUTS BEYOND 30O YOKE BECOMES STIFF AND IF RELEASED AT MORE THAN 30O, LEFT YOKE WILL STAY AT THAT POSITION UNTIL MANUALLY RETURNED TO ZERO. PROBLEM DID NOT OCCUR BELOW 10,000 FT ON CLIMB OR DECENT. REPLACED AILERON QUADRANT CENTERING SPRINApr 11, 1996 · N708DH · Boeing 72725 · Aileron Control SystemSDR 96FDEA00750Bulkhead · corrodedCORROSION (C53-100-01, 4) ON FWD SIDE OF 178 BULKHEAD, RBL 21-26 WL 218. CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED.Apr 8, 1996 · N154FE · Boeing 72725 · Fuselage Main, BulkheadSDR 96FDEA00751Side Frame · crackedFWD ENTRY DOOR, FWD SIDE FRAME IS CRACKED IN RADIUS ON LOWER EDGE, ADJACENT TO THE LOWER FWD STOP PIN FITTING. REMOVED FWD ENTRY DOOR CRACKED FWD SIDE FRAME, INSTALLED ONE EACH FWD SIDE FRAME IAW FEDEX 727 SRM 51-30-2 MM 52-11-01.Apr 6, 1996 · N154FE · Boeing 72725 · Passenger/Crew DoorsSDR 96FDEA00742Skin · gougedWHILE WORKING NR0152, FOUND THE FUSELAGE SKIN TO BE GOUGED AT BS 307 RBL 63 WL 249, ADJACENT TO THE FORWARD ENTRY DOOR FUSELAGE TORQUE TUBE. REMOVED DAMAGED AREA, REPAIRED SKIN IAW FEDEX SRM 53-30-3.Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00741Floor Beam · corrodedCORROSION (C53-224-01) ON LOWER SURFACE OF UPPER FLANGE OF FLOOR BEAM AROUND FASTENER HOLES BS 1110, RBL 10 TO 60 WL 208. REMOVED CORROSION FROM FLOOR BEAM, FOUND TO BE OUT OF LIMITS. ACCOMPLISHED FLOOR BEAM REPAIR BS 1110, RBL 10 TO 60 WL 208, IAW FEDEX SRMApr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00740Floor Beam · corrodedCORROSION (C53-224-01) ON FLOOR BEAM BS 344 LBL 45 AND RBL 37 WL 208. ACCOMPLISHED FLOOR BEAM REPAIR AT BS 344 LBL 45 AND RBL 37 WL 208, PER FEDEX SRM 27-53-007.Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00739Floor Beam · corrodedCORROSION (C53-224-01) ON FLOOR BEAM BS 380, LBL 28 TO 34 AND LBL 55 WL 208. REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS. ACCOMPLISHED FLOOR BEAM REPAIR PER FEDEX SRM 53-10-8.Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA00738Stringer · corrodedCORROSION (C53-113-01, 2) FOUND WHILE WORKING NR0602 STA 1055 STRINGER 28R IN STRINGER. FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, REMOVED DAMAGED AREA, REPAIRED STR 28R IAW FEDEX SRM 53-10-3.Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00760Skin · corrosionCORROSION (C53-132-02(1)). ON UPPER FUEL CELL AT BS 870, WL 190, RBL 44, RUNNING ORDER CAP. REMOVED CORROSION ON UPPER FUEL CELL SKIN AT BS 870, WL 190, RBL 44, AND REPAIRED DAMAGED SKIN PER FEDEX EA 7-5710-28189.Apr 4, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA00729Stringer · corrodedNR 0623, 042 CORROSION (C53-113-01, -2) FOUND WHILE WORKING NR0602 STA 1055 STR 28R IN STRINGER. *S/D* FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, REMOVED DAMAGED AREA REPAIRED STR 28R IAW FEDEX SRM 53-10-3.Apr 1, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00728Stringer · corrodedNR 0624 AND 043, CORROSION FOUND ON END OF STR SECTION STR 28R BS 1059.Mar 29, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA00723Bracket · corrodedLT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING IS CORRODED AROUND MAIN PULLEY BOLT HOLE AND TWO OTHER AREAS ON CASTING WBL 410. REMOVED CORRODED LT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING AND INSTALLED NEW CASTING IAW FEDEX MM 27-10-0,Mar 28, 1996 · N154FE · Boeing 72725 · Wing Miscellaneous StructureSDR 96FDEA00722Frame · corrodedWHILE WORKING ON NR 0412, FOUND CORROSION (7-5310-3364 PT 6) ON WINDOW FRAME AT BS 970 TO 990 ABOVE STR 11R. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED WINDOW FRAME AND INSTALLED NEW WINDOW FRAME AT BS 970 TO 990 STR 11R IAW SRM 53-10-1.Mar 28, 1996 · N154FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA00700Hinge Fitting · crackedNR0348 AND 030, RT WING O/B AILERON NR 3 HINGE FITTING IS CRACKED.Mar 25, 1996 · N154FE · Boeing 72725 · AileronsSDR 96FDEA00699Doubler · corrodedNR0611 AND 033, WHILE WORKING NR0602, FOUND DOUBLER TO HAVE CORROSION FROM BS 1050 TO 1125 FRONT STRINGER 26 TO 27R.Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA00698Beam · corrodedNR0486 AND 034, CORROSION (C53-224-01) ON LONGITUDINAL BEAM AND BARE METAL AROUND NUT CLIP HOLES LOWER SURFACE BS 780 TO 848 LBL 25.Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
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