Boeing 727-200

Service difficulty reports · 2,835

Newest first. General aviation reporting is voluntary.

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 04FDEA02449Stringer · dentedSTRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02448Stringer · dentedSTRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02447Stringer · dentedSTRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02446Stringer · dentedDENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02444Stringer · dentedDENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02443Stringer · dentedDENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02442Stringer · dentedDENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02445Stringer · dentedDENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02452Stringer · dentedSTRINGER DENTED AT BS 950 18, STRINGER 7 LT. *S/D* STR 7 LT ORIGINALLY FOUND OUT OF LIMITS (NO DENTS ALLOWED). REMOVED DENT BY BENDING EDGE OF STRINGER. MATERIAL LOSS A AS ALLOWABLE & STRINGER IS IN LIMITS PER SRM 53-10-1. ALODINED & PRIMED BLEND AREA PERAug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02455Floorbeam · corrodedCORROSION (C53-224-01, 1) FLOORBEAM STRUCTURE BS 344 LBL 31 TO LBL 58 WL 208. *S/D* REMOVED AND REPLACED UPPER FLOORBEAM CHORD AND REPAIR ANGLES AT BS 344, LBL 65-RBL 16, WL 208 IAW SRM 27-53-007.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02417Skin · corrodedCORROSION BS 1090, STR 29 LT- 29 RT. CUTOUT SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02416Skin · corrodedCORROSION ON SKIN, AFT CARGO BAY BILGE NEXT TO O/B SIDE OF STR 28L BS 994 LBL 22 WL 136. REMOVED DAMAGED AREA OF SKINA T BS 994. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3.Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02415Floorbeam · corrodedCORROSION AT FLOORBEAM BS 950D, LBL 10 DAMAGED, WL 208 (C53-224-01, 3). BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3.Aug 10, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02259Strip · damagedCOMPY WITH EA 7-7110-80586 POWERPLANT - COWL NR 3 ENG COWL RUB STRIP REPAIR P/N 259-0175-135. COMPLIED WITH EA 7-7110-80586.Jul 28, 2004 · N207FE · Boeing 727200 · Nacelle/Pylon, Main FrameSDR DHL2004749006Light · inoperativeON FORWARD INSTRUMENT PANEL, LE FLAPS INDICATOR HAS RT LIGHT INOP. EMERGENCY EXIT LIGHT OVER L-1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB, OPS CK GOOD IAW BMM CH 33-10-0, P/N 327. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD IAW BMM CH 33-50Jul 20, 2004 · N749DH · Boeing 727200 · Emergency LightingSDR C1HA200492016Warning Light · illuminatedAFTER DEPARTURE NR 1 ENGINE BYPASS INDICATOR ILLUMINATED. PERFORMED COM 2-72-19 PROCEDURE. RETURNED TO DFW CHANGED NR 1 ENG MAIN OIL FILTER REF MM 79-15-00. RAN ENG, INSPECTED FILTER, NO PARTICAL FOUND REF MM 71-00-00. INSPECTED NO DEBRIS NOTED REF P&W MM Jul 14, 2004 · N292CA · Boeing 727200 · Engine Indicating SystemSDR 04FDEA02043Support Fitting · corrodedCENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT FS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1.Jul 10, 2004 · N245FE · Boeing 727200 · Wing, Center BoxSDR 04FDEA02042Support Fitting · corrodedCENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT BS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1.Jul 10, 2004 · N245FE · Boeing 727200 · Wing, Center BoxSDR 04FDEA01860Fuel Tank · corrodedCORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821 RBL 13. *S/D* CORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821, RBL 13 REPAIRED PER EA NR 7-5730-55326.Jun 25, 2004 · N209FE · Boeing 727200 · Fuel StorageSDR 04FDEA01861Skin · dentedSTA 1037 ABOVE STR 23R SKIN IS DENTED. DENT AT BS 1037 STR 23 FOUND TO BE OUT OF LIMITS. REPAIRED DENT PER SRM 53-30-3 FIGURE 1.Jun 25, 2004 · N209FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA01742Floorbeam · corrodedCORROSION ON FLOORBEAM, STA 760, LBL 66, WL 206. *S/D* CORROSION OUT OF LIMITS. REMOVED STUB FLOORBEAM BS 760 LT SIDE. DRILLED UP & INSTALLED NEW STUB FLOORBEAM WL 200 PER SRM 51-30-2, 51-30-5, 53-10-1.Jun 15, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01741Frame · crackedFOUND FRAME BS 783 RT FASTENER HOLE CRACKED. REPAIR PER EO 7-5310-7-3367 PART 9. REPAIRED FRAME BS 783 RT PER EO 7-5310-7-3367 PART 9.Jun 15, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01706Control Unit · failedDISCHARGED BOTH LOWER CARGO COMPT FIRE BOTTLES, INDICATION OF FWD LOWER CARGO FIRE. AFTER CHECKING COMPARTMENT AND WHILE BEING TOWED HAD ANOTHER ACTIVATION OF LOWER CARGO FIRE WARNING. REMOVED AND REPLACED LWR FWD CARGO COMPT FIRE SUPP/SMOKE DET CONTROL ELECJun 13, 2004 · N270FE · Boeing 727200 · Fire DetectionSDR 04FDEA01705Frame · dentedAFT LWR CARGO COMPT FRAME 1010 UPPER FLANGE DENTED AT STR 26L. REPLACED FRAME IAW B727 SRM 51-40-3 FIG 1.Jun 12, 2004 · N244FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01704Shear Tie · corrodedFWD CARGO COMPT BILGE AREA HAS A CORRODED SHEAR TIE FS 520, STR 26L - 27L. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.Jun 12, 2004 · N244FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA01702Floorbeam · corrodedFLOORBEAM AND SHEAR WEB STA 1130, RBL 19 (TOP CHORD) EXFOLIATED. INSTALLED SEAT TRACK, 2 STRAPS AND T-CHORD IAW SRM 51-30-2. INSTALLED REPAIR IAW SRM 53-10-8.Jun 12, 2004 · N244FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01701Intercostal · corrodedAFT LWR CARGO COMPT INTERCOSTAL INBOARD OF STR 26L, BETWEEN FS 1140 TO 1166, UPPER AND LWR FLANGES CORRODED. INSTALLED FABRICATED FLANGES OF INTERCOSTAL IAW SRM 51-30-2. INSTALLED FABRICATED DOUBLER AT STA 1140 -1166, STR 26L IAW SRM 51-30-2.Jun 12, 2004 · N244FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01696Control Unit · malfunctionedFORWARD LOWER CARGO COMPARTMENT FIRE INDICATION ON TAXI OUT. NO ACTUAL FIRE REPORTED BY FIRE DEPARTMENT AFTER FIRE BOTTLES DISCHARGED INTO FWD LOWER CARGO COMPARTMENT. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES AND THE CARTRIDGES PER MM 26-17-014-Jun 11, 2004 · N270FE · Boeing 727200 · Fire DetectionSDR 04FDEA01631Frame · dentedFWD CARGO BAY STA 680 FRAME DENTED STR 25 LT.Jun 7, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01630Floorbeam · corrodedCORROSION ON FLOORBEAM STRAP AT BS 950, LBL 9, WL 138.Jun 7, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01629Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 950, RBL 27.5, WL 208 UPPER FLANGE.Jun 7, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01619Structure · corrodedCORROSION AT LOWER SURFACE OF CTR FUEL TANK, BS 830, RBL 26, WL 160, JUST ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION AT LOWER SURFACE OF CENTER FUEL TANK - BS 830, RBL 26, WL 160 ABOVE PRIMARY HEAT EXCHANGERS FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. REPAIJun 4, 2004 · N222FE · Boeing 727200 · Fuel StorageSDR 04FDEA01605Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 950 RBL 27.5 WL 208 UPPER FLANGE. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-6 AND FED EX EA 7-5310-55308.Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01604Floorbeam · corrodedWHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 1070, LBL 25 TO RBL 60, WL 200 LOWER FLOORBEAM FWD SIDE CORRODED. REPAIRED FLOOR BEAM BS 1070 PER FED EX EA 7-5310-55306.Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01603Frame · damagedBS 990 FRAME LT PREVIOUS REPAIR CRACKED ON BOTTOM. FOUND DAMAGE TO BS 990 FRAME, STR 24 LT TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 51-40-3 AND FED EX EA 7-5310-55307.Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01602Frame · dentedSIDE FRAME DENTED BS 460 RBL 65 STR 16R. FOUND DENT IN 460 FRAME, STR 16R TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665A.Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01601Floorbeam · corrodedCORROSION (C53-224-04) ON FLOORBEAM AROUND NUT PLATE HOLES BS 1130, LBL 27 - LBL 43, WL 207. CORROSION OUT OF LIMITS. REPAIRED 1130 FLOORBEAM UPPER CHORD LBL 27-43 WL 207 IAW SRM 53-10-8 FIG 10.Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01566Floorbeam · corrodedWHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 970 LBL 12 WL 200 LOWER FLOORBEAM CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED FLOORBEAM LOWER CHORD 1 X 4.25 INCHES. FABRICATED & INSTALLED REPAIR ANGLES (2 EA) & FILLER, AND RESTORED ALL ACCESS PER SRMJun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01565Floorbeam · corrodedCORROSION (C53-224-01) FLOORBEAM UPPER FLANGE LWR SURFACE IS GOUGED AND CORROSION STA 400 LBL 2-8 WL 208. REPAIRED FLOORBEAM AT BS 400, LBL 2-8, WL 208 IAW SRM 53-10-8 FIG 3, 51-40-3, 51-10-3, FED EX MM 51-20-000-7, 51-20-021-7, SRM 51-30-2. ORIGINAL MATERIAJun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01564Floorbeam · corrodedCORROSION (C53-224-01, 3) FLOORBEAM STA 1130 LWR CHORD FWD FLANGE UPPER SURFACES CORRODED LBL 1-45 WL 200 AROUND NUT PLATE. REMOVED CORROSION ON 1130 FLOORBEAM, LOWER CHORD, FWD FLANGE UPPER AND LOWER SURFACES LBL 1 - LBL 45, WL 200 AROUND FASTENER HOLES. ORJun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01563Stringer Clip · crackedFWD CARGO COMPARTMENT STA 520 WL 150 RBL 21 STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 520, WL 150, RBL 21, STR 26R. REMOVED DAMAGE 1 X 5 INCH FROM EDGE OF CLIP. ALODINED AND PRIMED BARE METAL IAW SRM 51-30-2, 51-10-01, 51-10-2.Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01562Frame · dentedFWD CARGO COMPARTMENT STA 560 WL 155 LBL 35 FLOOR FRAME DENTED. CUT OUT DAMAGE IN FRAME AT BS STA 560 WL 155 LBL 35 AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1.Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01561Failsafe · corrodedCORROSION (C53-224-01, 2) ON FRAME, STA 760, RBL 70, WL 207. FOUND CORROSION ON FRAME FAIL SAFE STRAP AT BS 760 RBL 70, WL 207 TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED DAMAGED SECTION OF FAIL SAFE STRAP. FABRICATED REPAIR SECTION OF STRAP AND DOUBLER PJun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01499Frame · dentedFWD CARGO COMPARTMENT STA 520, WL 163, LBL 39 FRAME DENTED. REMOVED DAMAGE ON FRAME B.S. 520, WL 163, LBL 39 IN A 1 1/2 X 17 1/2 AREA. FABRICATED REPAIR DOUBLER USING 7075-T6 .050 LOT 553781. ALODINED, PRIMED AND INSTALLED IAW 727 SRM 51-30-2, 51-40-3 SH3 AMay 27, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01498Floorbeam · corrodedCORROSION (C53-224-01,3) FLOORBEAM STA 1110 WL 208 CORRODED UPPER CHORD. REMOVED CORROSION FROM BS 1110 FLOOR BEAM, FOUND TO BE OUT OF LIMITS PER SRM 53- 10-1. ACCESSED AREA, REPLACED UPPER CHORD PER FED EX EA 7-5310-77727, RESTORED ACCESS PER SRM 51-30-2 AMay 27, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01465Stringer Clip · crackedCRACKED STRINGER CLIP, STA 950C, STRINGER 3L. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3L IAW SRM 51-30-2.May 26, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01464Frame · dentedFRAME UPPER CHORD DENTED BS 1010, RBL 30 ABOVE STR 26R. CUT OUT DAMAGED AREA OF FRAME AT BS 1010, RBL 30 ABOVE STR 26R IN 1.75 X 1.5 DIAMETER AREA. FABRIATED TYPICAL FORMED SECTION REPAIR. ALODINED, PRIMERED AND INSTALLED IAW SRM 51-40-3 FIGURE 1, SRM 51-10-May 26, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01446Stringer Clip · crackedSTRINGER CLIP CRACKED STA 950B STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 950B, STR 7R IAW SRM 51-30-2.May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01445Frame · dentedFWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FLOOR FRAME DENTED. FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FRAME DENTED OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665.May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01444Frame · dentedSTA 600 FRAME DENTED BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY. FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY DENT FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665.May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame
Back to Boeing 727-200