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 04FDEA01443Frame · dentedFWD CARGO BAY STA 660 FRAME DENTED AT STR 24 LT. REPAIRED DENTED FRAME AT FWD CARGO BAY STA 660, STR 24L IAW EA 7-5310-70665 AND SRM 51-40-3.May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01442Frame · dentedFWD CARGO STA 680 FRAME DENTED AT STR 24 RT. CUT OUT DAMAGE ON FRAME INNER CHORD BS 680, STR 24 RT. DRILLED UP REPAIR DOUBLER AND INSTALLED PER SRM 51-40-3 FIG 1 AND FED EX EA 7-5310-70665.May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01447Connector · disconnectedDURING DESCENT AT FL 280 NR 2 ENGINE OIL TEMP INCREASED TO 135, FOLLOWED QRH PROCEDURES FOR HIGH OIL TEMP, OIL TEMP REMAINED IN YELLOW BAND. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AFTER 15 MINUTES WITH OIL TEMP STILL IN YELLOW BAND. NR 2 ENGINE WAS SHUTDOWNMay 25, 2004 · N281FE · Boeing 727200 · Fuel HeaterSDR FX72004F00002Accessory Unit · malfunctionedAFTER T/O AND AFTER GEAR RETRACTION, LT MAIN GEAR RED LIGHT STAYED ON, RECYCLED GEAR DID NOT SOLVE PROBLEM AC RETURNED WITHOUT INCIDENT. T/S SYSTEM REPLACED LANDING GEAR ACCY. PERFORMED GEAR SWING IAW MM AND LANDING GEAR ACCY UNIT IAW MM. SYSTEM CHECKS GOODMay 24, 2004 · N211DB · Boeing 727200 · Landing Gear Retraction/Extension SystemSDR 04FDEA01435Floorbeam · corrodedCORROSION (C53-224-01) ON FLOORBEAM UPPER SURFACE BS 380 RBL 25 TO 35 WL 208. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA RBL 25.75 TO 27.75 AND RBL 46 TO 48 AT BS 380, WL 208. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS, BOTMay 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01434Stringer Clip · crackedCRACKED STRINGER CLIP, STA 950D, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 6R IAW SRM 51-30-2.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01433Stringer Clip · crackedCRACKED STRINGER CLIP, STA 950C, STRINGER 5R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 5R IAW SRM 51-30-2.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01432Stringer Clip · crackedCRACKED STRINGER CLIP, STA 950C, STRINGER 3R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3R IAW SRM 51-30-2.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01428Floorbeam · corrodedCORROSION (C53-224-01), ON FLOORBEAM LWR FLANGE STA 600 RBL 49 TO 60 WL 201. REMOVED CORROSION ON LOWER FLANGE FLOORBEAM CHORD AT BS 600, RBL 49-60, WL 201. FOUND TO BE OUT OF LIMITS. ACCESSED AREA AND CUT LOWER CHORD FROM RBL 35 TO END OF FLOORBEAM. FABRIMay 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01427Floorbeam · corrodedCORROSION (C53-224-01), ON FLOORBEAM BS 344 LBL 33 TO 60 WL 208 AROUND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM, BS 344. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, RBL 65 - LBL 65, WL 208. ALLMay 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01426Frame · dentedFWD CARGO STA 660 FRAME DENTED AT STR 24 RT. TRIMMED OUT DENT DAMAGE FROM FLANGE ON FRAME STA 660, STR 24R, LOCATED AND DRILLED FASTENER HOLES IN REPAIR DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7-5310-70665. ALODINED, PRIMERED AND INSTALLED FASTENERS PER SRM 51May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01425Stringer Clip · crackedSTRINGER CLIP CRACKED STA 950A STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 7R IAW SRM 51-30-2.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01424Stringer Clip · crackedSTRINGER CLIP CRACKED STA 950C STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 7R IAW SRM 51-30-2.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01423Stringer Clip · crackedSTRINGER CLIP CRACKED STA 950A STR 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 6R IAW SRM 51-30-2.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA01422Floorbeam · corrodedFLOORBEAM TOP TEE CORRODED STA 1030 LBL 25 - RBL 25 WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMGE AREA PER SRM 53-10-8.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA01421Stringer · corrodedFWD CARGO STR 26 RT STA 720B CORRODED. REMOVED DAMAGE AREA OF STRINGER AND STIN AT BS 720B. FABRICATED AND INSTALLED REPAIRS IAW SRM 53-30-3, 53-10-3.May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA01412Bracket · gougedWINGS - SPOILERS - SPOILER DOWN STOP BRACKET GOUGE REPAIR. COMPLIED WITH EA 7-5740-77411. BLENDED GOUGE, HFEC NO CRACKS NOTED.May 22, 2004 · N241FE · Boeing 727200 · SpoilersSDR 04FDEA01388Stringer Clip · crackedSTRINGER CLIP CRACKED STA 950D STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 7R IAW SRM 51-30-2.May 21, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 04FDEA01392Position Switch · failedNR 1 L/E FLAP FAILED TO RETRACT AFTER T/O. FOLLOWED RED TABS AND RETURNED TO LAND. REMOVED AND REPLACED NR 1 L/E FLAP POSITION SWITCH PER MM 27-82-001-4. OPS CHECK GOOD PER MM. ACFT OK FOR SERVICE.May 21, 2004 · N276FE · Boeing 727200 · Leading Edge Slat Position Indicating SystemSDR 04FDEA01387Rib · damagedCOMPLY WITH EA 7-5720-77412 WING - SPOILER DOWN STOP RIB REPAIR. COMPLIED WITH EA 7-5720-77412. WORKED IN CONJUNCTION WITH EA 7-5720-77423.May 21, 2004 · N241FE · Boeing 727200 · Wing, Rib/BulkheadSDR 04FDEA01382Shear Tie · corrodedCORROSION (C53-111-01, 2) FWD CARGO BAY SHEAR TIE ON FRAME 720 STR 26 LT IS CORRODED. REMOVED CORROSION ON SHEAR TIE ON FRAME STA 720, STR 26 LT, FWD CARGO BAY. REMOVED .017 3 X 1 INCH FROM .050, OUT OF LIMITS. REMOVED DAMAGED SHEAR TIE, LOCATED, DRILLED, IMay 21, 2004 · N222FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA01378Shear Tie · corrodedAFT CARGO COMPT HAS A CORRODED SHEAR TIE AT FS 970 STR 28L - 29L. FABRICATED SHEAR TIE ON TRAVELER T4/432278 & FABRICATED FLOOR SUPPORT ON TRAVELER T4/430988. REPAIRED & INSTALLED SHEAR TIE AT FS 970 STR 28L - 29L IAW SRM B727 SRM 53-10-4 PAGE 46.May 20, 2004 · N241FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA01377Floor Support · corrodedFWD PIT - STA 715 FLOOR SUPPORT R3 - EXFOLIATED AT NUT PLATE HOLES. FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-4, INSTALLED IAW SRM 51-30-2, ON NON ROUTINE N00637 AT MAE.May 20, 2004 · N241FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01376Floor Support · corrodedFWD PIT - STA 715 - FLOOR SUPPORT L2 EXFOLIATED AT NUT PLATE HOLES. FABBED NEW FLOOR SUPPORT ON TRAVELER T4/430748 & INSTALLED REPAIR IAW SRM 51-40-4 AND 51-30-2, ON NON ROUTINE N00641 AT MAE.May 20, 2004 · N241FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01344Frame · dentedFWD CARGO STA 629 FRAME DENTED LBL 6 STR 28. CUT OUT DAMAGED PORTION OF FRAME AT BS 720 LBL 6 STR 28 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3.May 19, 2004 · N222FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA01345Stringer · corrodedCORROSION ON STRINGER 27R BS 955. REMOVED AND REPLACED STR 27 RT IN ACCORDANCE WITH FED EX E.A #7-5310-55318.May 19, 2004 · N222FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA01331Stringer · crackedRIGHT MLG W/W - CRACK IN STR 18 AT APPROX STA 908. STOP DRILLED CRACK AS PER SRM 53-10-1 FIG 1. FABRICATED REPAIR ANGLES ON MAE TRAVELER T4/428590. INSTALLED REPAIR ANGLES IAW SRM 51-30-2, ON NON ROUTINE N00097.May 18, 2004 · N241FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA01330Support Angle · crackedNR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE HAS A CRACK. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE IAW SRM 51-30-2, ON NON ROUTINE N00606.May 18, 2004 · N241FE · Boeing 727200 · Drag Control ActuatorSDR 04FDEA01329Stringer · corrodedFWD PIT - STA 720E - 720F, STR 27L EXFOLIATED. CUT OUT STRINGER DAMAGE IAW SRM 53-10-3 FIG 1, FABRICATED NEW SECTION STRINGER & REPAIR SPLICES FROM MAT BAC 1498-147, BATCH 32659 & BAC 1498-131 BATCH 54832 IAW SRM 53-10-3. INSTALLED STRINGER & SPLICES IAW SRMMay 18, 2004 · N241FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA01275Battery · dischargedCOCKPIT EMERGENCY EXIT LIGHT REMAINS ON. INSTALLED NEW BATTERIES IN COCKPIT EMERGENCY LIGHT ASSY PER STD MX PRAC & SECURED LIGHT BRACKET WHICH WAS STARTING TO COME LOOSE. EMERGENCY LIGHTS OPS CHECK NORMAL.May 15, 2004 · N491FE · Boeing 727200 · Emergency LightingSDR 04FDEA01274Battery · dischargedFORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. INSTALLED RECHARGED BATTERIES INTO EMER LIGHT UNIT IAW PART 33-50-00 OF AMM. OPS CHECK NORMAL.May 14, 2004 · N266FE · Boeing 727200 · Emergency LightingSDR 04FDEA01270Transition Panel · corrodedFWD PIT - LT TRANS PANEL STR 675 - 2 NUT PLATE HOLES EXFOLIATED. REMOVED & REPLACED TRANS ANGLE IAW SRM 51-30-2. ORIGINAL TRANS ANGLE .050. REMOVED .050 IAW SRM 51-10-6. REMAINING .000 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 PG 2. FABRICATED NEW TRANS ANGLE FMay 14, 2004 · N241FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01253Hinge · wornCOMPLY WITH EA 7-5210-77407; DOORS - MAIN CARGO DOOR HINGE WEAR REPAIR P/N B27-53-070-03. COMPLIED WITH EA 7-5210-77407. MAIN CARGO DOOR HINGE REPAIR P/N B27-53-070-03.May 13, 2004 · N241FE · Boeing 727200 · Cargo/Baggage DoorsSDR 04FDEA01251Intercostal · corrodedAFT CARGO COMPT FS 1147 - 1164 STR 27L - STR 28L INTERCOSTAL HAS LIGHT CORROSION AND MISSING NUT PLATES ON LWR SURFACE OF CHORD. REMOVED CORROSION IAW SRM 51-10-6, OUT OF LIMITS IAW SRM 53-10-1, REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-May 13, 2004 · N241FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01217Clip · corrodedFWD PIT - STA 720D, FRAME FOR BULKHEAD PANEL, BOTTOM SIDE CLIP CORRODED RBL 4. REMOVED CLIP IAW SRM 51-30-2, FABRICATED NEW CLIP IAW SRM 51-20-1, MAE MATERIAL ID 04074,7075-T6 .032 BATCH 671070, INSTALLED NEW CLIP IAW SRM 51-30-2, AT MAE.May 11, 2004 · N241FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 277847Pump · leakingDURING CRUISE FLIGHT, EXPERIENCED A LOSS OF HYDRAULIC FLUID ON (B) SYSTEM. AN EMERGENCY LANDING WAS INITIATED AND THE AIRCRAFT LANDED, WITHOUT INCIDENT. REMOVED AND REPLACED B SYSTEM HYDRAULIC PUMP.May 8, 2004 · N7635U · Boeing 727200 · Hydraulic Pump, AuxiliarySDR 04FDEA01167Bracket · crackedRIGHT MLG DOOR FORWARD HINGE SEAL SUPPORT THE AFT BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, FABBED FROM 2024-T3 .040 BATCH 744347 AT MAE ON N/R N00389.May 8, 2004 · N241FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01142Door Frame · crackedWHILE PERFORMING MAIN CARGO DOOR OPS CHECK FOUND AFT DOOR FRAME BS 618, WL 228 TO BE CRACKED. REMOVED DAMAGE IN MCD AFT FRAME BS 618, WL 228. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS AND FASTENERS REMOVED FOR ACCESS. ALL WORK DONE IAW SRM 51-40-3 May 3, 2004 · N243FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA01114Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4.Apr 29, 2004 · N206FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA01113Rib · crackedRIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1.Apr 29, 2004 · N206FE · Boeing 727200 · Wing, Rib/BulkheadSDR 04FDEA01115Skin · crackedLOWER FUSELAGE EXTERIOR SURFACE, SKIN CRACKED AT STATION 1010 AT APPROX STR 29R WITH CORROSION. CUT OUT DAMAGED SECTION OF SKIN IAW SRM 53-30-3 FIG 3A, FABRICATED AND INSTALLED (1) EA DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3A AT MAE.Apr 29, 2004 · N206FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA001114Floor Support · crackedFWD CARGO COMP'T FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4.Apr 29, 2004 · N206FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA001113Rib · crackedRIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1.Apr 29, 2004 · N206FE · Boeing 727200 · Wing, Rib/BulkheadSDR 04FDEA01112Structure · gougedCOMPLY WITH EA 7-5750-77346; WINGS - LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE.Apr 28, 2004 · N206FE · Boeing 727200 · Leading Edge DevicesSDR 04FDEA001112Skin · gougedCOMPLY WITH EA 7-5750-77346; WINGS, LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE.Apr 28, 2004 · N206FE · Boeing 727200 · Leading Edge DevicesSDR 2004F00109Brake · damagedNEWLY MANUFACTURED, BRAKES WERE REMOVED, AFTER MAINTENANCE INSPECTION REVEALED BRAKE WAS COMING APART BETWEEN HEAT STACK AND PISTON HOUSING ASSEMBLY INTERFACE.REVIEW AT REPAIR FACILITY FOUND: 7 OF 8 TIE BOLTS WERE MISSING OF BRAKE SERIAL B4874. POSITION NR 1. Apr 28, 2004 · Boeing 727200 · Landing Gear Brake SystemSDR 04FDEA01105Seat Track · corrodedMAIN CARGO COMPT SEAT TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACED SEAT TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2.Apr 26, 2004 · N206FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA001105Cargo Track · corrodedMAIN CARGO COMPT CARGO TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACED CARGO TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2.Apr 26, 2004 · N206FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01103Splice · corrodedCOMPLY WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE CORRODED. COMPLIED WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE.Apr 25, 2004 · N206FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01286Brake · blownON BLOCK, FOUND NR 1 BRAKE ASSY BLOWN APART.Apr 23, 2004 · N216FE · Boeing 727200 · Master Cylinder/Brake Valve
Back to Boeing 727-200