N272FE, cancelled Nov 28, 2007

Service difficulty reports · 41

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N272FE' AND deregistration_id = 'N272FE-2007-11-28'
  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 05FDEA01778Seat Track · corrodedSEAT TRACK LBL 24 HAS CORROSION AT 500 TO 520 AND STA 620. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5 FIG 1 PG 4Jul 2, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01776Tee Fitting · corrodedTEE CHORD 760 -787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE CHORD IAW SRM 51-30- 2Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01775Tee Fitting · corrodedTEE FITTING APPROX STA 760-787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE FITTING IAW SRM 51-30-2Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01774Seat Track · corrodedSEAT TRACK STA 740-760 LBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-1.Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01748Seat Track · corrodedSEAT TRACK LBL 24 IS CORRODED 690 - 740. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-30-2Jun 30, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01747Seat Track · corrodedSEAT TRACK STA 480 - 690 AT LBL 45 HAS CORROSION . REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2Jun 30, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01718Frame · chafed344 FRAME CHAFED AT STR'S 4R,6R & 8R. FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 51-40-3Jun 28, 2005 · N272FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA01666Seat Track · corrodedSEAT TRACK LBL 24 HAS CORROSION FROM STA 344-480. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.Jun 23, 2005 · N272FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01508Hydraulic Line · rupturedA-HYD SYSTEM FLUID LOSS / ISOLATED TO -A- PUMP NR 2. AFTER SHUTDOWN, THE -A- SYSTEM QTU. READ 2.5 GALLONS AND THE FLUID SHUTOFF SWITCHES WERE NOT TURNED OFF. OPENED COUPLING AND MOTORED ENGINE. FOUND PRESSURE LINE FROM THE PUMP TO THE FIREWALL RUPTURED.Jun 2, 2005 · N272FE · Boeing 727200 · Hydraulic System, MainSDR 05FDEA00964Bushing · looseBUSHINGS LOOSE ON UPPER CLEVIS FOR THE PCU ROD END. REPAIRED UPPER RUDDER CLEVIS BUSHINGS FOR THE PCU RODEND IAW FED EX EA 7-5530- 86276.Apr 11, 2005 · N272FE · Boeing 727200 · Vertical Stabilizer Miscellaneous StructureSDR 05FDEA00921Skin · damagedRIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE IS GOUGED AND BENT AT NR 7 CARRIAGE. REPAIRED RIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE AT NR 7 FLAP CARRIAGE PER EA 7-5710-86274.Apr 10, 2005 · N272FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA00920Rib · chafedVERTICAL STAB T/E CAVITY RIB WEB IS CHAFED AT UPPER SURFACE, FIN STA 180, 5 RBL, THROUGH ACCESS PNL 9510. REPAIRED THE CHAFED RIB WEB, VERTICAL STAB T/E CAVITY AT UPPER SURFACE FIN STA 180, 5 RBL IAW FEDEX EA 7-5530-86275.Apr 10, 2005 · N272FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 05FDEA00872Skin · lightning strikeLIGHTNING STRIKE ON CROWN BS 588 BETWEEN STR 1 AND STR 2L. FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW FED EX EA 7-5330-866368.Apr 6, 2005 · N272FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA00847Skin · crackedCRACKED EXTERNAL SKIN FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED CRACK PER FED-EX EA 7-5330-86273.Apr 5, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA00834Stringer Clip · corrodedCORROSION C53-113-01 (1) UNDER LEVELING COMPOUND BS 660 STR 28R. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS, REPAIRED DOUBLER, SHEAR TIE PER SRM 53-10-4, 53-30-3.Apr 4, 2005 · N272FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA00832Skin · dentedDENT IN EXTERNAL FUSELAGE SKIN AT BS 1345 BY LEFT AFT CORNER OF AIRSTAIR CUT OUT. REPAIRED DENT PER SRM 54-30-3.Apr 4, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA00779Housing · gougedNR 3 LOWER CARGO DOOR, HANDLE HOUSING GOUGED BY HANDLE STUD. REMOVED AND REPLACED #3 LWR CARGO DOOR HANDLE PER SRM 51-30-02.Apr 1, 2005 · N272FE · Boeing 727233 · Cargo/Baggage DoorsSDR 05FDEA00735Shear Web · corrodedCORROSION IN SHEAR WEB BS 1166 LBL 29-33 WL 208.Mar 31, 2005 · N272FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA00736Support · corrodedLWR FUSELAGE, BS 740 R A/C BAY RBL 10, CORROSION EMANATING FROM LWR CHORD AND BULKHEAD. REPAIRED BS470 LOWER CHORD PER FED-EX EA 7-5310-86268.Mar 31, 2005 · N272FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 05FDEA00691Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED AT NR 3 CARGO DOOR CUTOUT, BS 1096 AT STR 24R. REPAIRED GOUGE PER FED-EX EA. 7-5330-86272.Mar 29, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA00662Skin · damagedEXTERNAL FUSELAGE SKIN HAS FOD/GRAVEL DAMAGE, BS 480-520, STR 22R-27L ALONG BELLY SKIN. RVSM CRITICAL AREA. REPAIRED SKIN BS 496-501 AT STR 27R PER SRM 53-30-3.Mar 28, 2005 · N272FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA00635Bulkhead · corrodedLOWER CHORD OF BS 950 CANTED BULKHEAD IS CORRODED, RBL 23. REPLACED BS 950 LOWER CHORD PER SRM 51-40-3 & 51-30-2.Mar 25, 2005 · N272FE · Boeing 727200 · Fuselage Main, BulkheadSDR 05FDEA00632Shear Tie · corrodedCORROSION ON SHEAR TIE FWD SIDE AT BS 1030, JUST OB OF STR 28 LT, AFT CARGO BAY. REPAIRED PER SRM 53-10-4.Mar 24, 2005 · N272FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 02FDEA00725Stringer · dentedDENT IN STR FLANGE AT BS 492, STR 23L. R&R STR FLANGE PER SRM 53-10-1, 53-10-3.Oct 12, 2002 · N272FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 02FDEA00724Skin · corrodedCORROSION ON SKIN LAP AT SHEAR TIE AT BS 720B, STR 26R. R&R SKIN PER SRM 53-10-5, 51-30-2, 51-30-5.Oct 12, 2002 · N272FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00729Frame · dentedFRAME DENTED AT BS 500, STR 23R - 24R. R&R FRAME PER SRM 51-40-3.Oct 12, 2002 · N272FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00728Skin · dentedDENT ON SKIN AT BS 465 BELOW STR 16R. R&R SKIN PER SRM 53-30-1, 53-30-3.Oct 11, 2002 · N272FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00747Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 45-55, WL 208. R&R UPPER CHORD PER ER 02-1505.Oct 8, 2002 · N272FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00726Seat Track · corrodedCORROSION ON SEAT TRACK I/B FLANGE UPR SURFACE AROUND NUTPLATE HOLES AT BS 760-848, LBL 24, WL 208. R&R SEAT TRACK PER SRM 51-30-2.Oct 8, 2002 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00730Skin · bulgedBULGING ON BELLY SKIN BETWEEN BS 1050 TO 1060, LBL 20. R&R SKIN PER SRM 53-30-1, 53-10-1, 53-30-3.Oct 7, 2002 · N272FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 01FDEA00226Landing Gear · malfunctionedLANDING GEAR FAILED TO RETRACT. RAN CKLIST, CK CB AND WAS NOT POPPED, ATTEMPT 2ND RETRACT AND WAS SUCCESSFUL. PERF LG HANDLE LOCK SYS ADJUSTMENT AND TEST PER 727-200 MM 32-31-011-5. CK OK. NO BINDING OR STICKING NOTED DURING ACTUATION.Mar 23, 2001 · N272FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 99FDEA00310Overheat Sensor · malfunctioned99-190 - NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. EMERG PROC ACCOMPLISHED. LIGHT REMAIN ILLUM. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 3 ENGINE STRUT OVERHEAT SENSING ELEMENT PER MM 26-14-001-2, RAN ENG PER JET RUN HANDBOOK OPER CK GOOD. NO PNEUMATIC LEAKS Aug 4, 1999 · N272FE · Boeing 727233 · Overheat DetectionSDR 99FDEA00300Control Unit · failed99-185 - NR 3 ENG STRUT OH LIGHT ILLUMINATED, RAN RED TABS CKLIST. REMOVED AND REPLACED FIRE AND HEAT DETECTION CONTROLLER, PER MM 26-14-000-1. OPS CK GOOD.Jul 30, 1999 · N272FE · Boeing 727233 · Fire DetectionSDR 97FDEA00751Floorbeam · corodedNR 0621 GEN NR 72C237-02, BS 950 FLOORBEAM CAP LBL 45 TO LBL 55 HAS CORROSION ON TOP AND AROUND NUTCLIP HOLES INSTALLED STRAP IN ACCORDANCE WITH EA 7-5310-29241 DATED 10/7/97.Oct 14, 1997 · N272FE · Boeing 727223 · Fuselage Main, Floor BeamSDR 97FDEA00749Frame · dentedNR 0572, LWR AFT CARGO, DENT IN FRAME 1010 ABOVE STR 25R, CUT OUT DAMAGE. INSTALLED REPAIR PER SRM 53-10-4.Oct 11, 1997 · N272FE · Boeing 727233 · Fuselage Main, FrameSDR 97FDEA00740Chord · crackedCRACK IN FWD LWR FLANGE OF 2ND CHORD FWD OF RT WING REAR SPAR, INSIDE FUEL CELL AT WS 686.5. INSTALLED DOUBLER PER BOEING SB NR 727-57A159.Oct 10, 1997 · N272FE · Boeing 727233 · Wing Miscellaneous StructureSDR 97FDEA00739Chord · mismanufacturedRT WING, WS 686.5, AFT SIDE OF 2ND CHORD, FWD OF REAR SPAR HAS AREA WHERE TOO MUCH MATERIAL (TAK). REMOVED NEXT TO DOUBLE FLUSH RIVET. BLENDED OUT AREA PER SRM 51-10-1 PG 2 AND PER SB 727 57A159. ALODINED AND PRIMED PER M/M 51-20-1. INSTALLED REPAIR PER EAOct 10, 1997 · N272FE · Boeing 727233 · Wing Miscellaneous StructureSDR 97FDEA00750Seat Track · corrodedNR 0643 GEN NR 72C237-02 BS 1015, LBL 25 SEAT TRACK HAS CORROSION BETWEEN LUGS AND ON TOP OF LUGS. REMOVED AND REPLACED OLD SEAT TRACK WITH NEW ONE PER SRM 51-10-1.Oct 8, 1997 · N272FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 97FDEA00700Skin · damagedNR 1 CARGO DOOR CUTOUT BS 600 FUSELAGE SKIN, DOUBLER AND TRIPLER DAMAGED AT LWR CUTOUT. *S/D* INSTALLED DOUBLERS AND FILLER IN CARGO DOOR CUTOUT PER EA 75-330-29236 DATED 10-03-97.Oct 1, 1997 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00180Bypass Valve · failedON LANDING APPROACH, O/B FLAPS DIDN'T EXTEND WITH FLAP HANDLE, I/B FLAPS OKAY. SUBSEQUENT SYSTEM-A HYD HAD TOTAL LOSS. CHECKLIST, M/GAR EXTENSION AND LANDED OKAY. FOUND O/B TRAILING EDGE BYPASS VALVE BODY SEPARATED. REMOVED AND REPLACED VALVE, LEAK CHECKS Feb 3, 1996 · N272FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 95FDEA01594Apu · fireGROUND CREW REPORTED, APU W/N LIGHT OFF OR SHUTDOWN, RESIDUAL FUEL IGNITED CAUSING FIRE AND FIRE BOTTLE DISCHARGED. STARTED APU 3 TIMES, OPS CK GOOD. APU SHUTDOWN NORMALLY WITH MASTER SW OR FIRE HANDLE. SUSPECT NO LIGHT ON APU WAS CAUSED BY COLD SOAKED APU.Oct 25, 1995 · N272FE · Boeing 727233 · Airborne Auxiliary Power Unit (APU) System
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