N237FE, cancelled Dec 19, 2013

Service difficulty reports · 55

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 = 'N237FE' AND deregistration_id = 'N237FE-2013-12-19'
  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 FDEA201104051330Oil System · leakingAIRCREW WROTE UP OIL QUANTIY IN NR 2 PRIOR TO FLT STARTED WITH 4 1/2 GALLONS. QUANTIY WAS 2 1/2 GALLONS STARTING CRUISE. AFTER APPROXIMATELY 40 MINUTES OIL OUANTY WAS ZERO. COMPLIED WITH RED TABS DURING CRUISE. SHUTDOWN NR 2 ENGINE WHEN PRESSURE DROPPED IN TApr 5, 2011 · N237FE · Boeing 727247 · Turbine Engine Oil SystemSDR FDEA200902210628Keelbeam · corroded29R KEEL BEAM AT STA.950C TO 950E IS CORRODED. REPAIRED KEELBEAM AREA AT STA 950C-950E BY REMOVING CORROSION AND INSTALLED STRAP REPAIR IAW EA NR 7-5310-124065.Feb 21, 2009 · N237FE · Boeing 727247 · Fuselage Main, KeelSDR FDEA200902210627Stringer · corrodedLOWER FWD CARGO COMPARTMENT HEAVY CORROSION ON SKIN LAP, STR 26R FROM 720D - 720E 18 AND FRAME FS 720E AT 26R REPAIRED STR 26 FROM 720D-740 IAW SRM 53-10-3 FIG I. REPAIRED SKIN AT LAP JOINT STA 720D-720E IAW SRM 53-30-3 FIG 24.Feb 21, 2009 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FDEA200902210626Stringer · corrodedAT STA 720D LT SIDE STR 22L HAS LIGHT CORROSION. REPAIRED STRINGER 22L STA 720D LT SIDE IAW SRM 53-10-3 FIG 1, REPAIR PART FABRICATED ON TRAVELER T8/781589.Feb 21, 2009 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FDEA200902210625Structure · crackedLT WING T/E COVE AREA FALSE SPAR WEB CRACKED OTBD OF NR 7 SPOILER ACTUATOR. REPAIRED SPAR WEB IAW SB 727-57-158 PARTS FABRICATED ON TRAVELERS T9/780969,T9/780970,T9/780968,T9/780971,AND T9/780967. REPAIR DOUBLER FABRICATED.Feb 21, 2009 · N237FE · Boeing 727247 · Wing Miscellaneous StructureSDR FDEA200902180573Seat Track · crackedMAIN DECK SEAT TRACK EXT EXTENSION AT STA.850-870 RBL 45-63 CRACKED . REMOVED SEAT TRACK EXTENSION AND BUSHINGS IAW SRM 51-30-2. FABRICATED SEAT TRACK EXTENSION IAW DWG 69-24621. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK EXTENSION AND BUSHIFeb 18, 2009 · N237FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902100500Shear Tie · corrodedLOWER FWD CARGO COMPARTMENT, FRAME SHEAR TIE CORRODED AT FS 720F BETWEEN STR 26 AND 27 L. REMOVED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE ON MAE TRAVELER NR T9/780298.Feb 10, 2009 · N237FE · Boeing 727247 · Fuselage Internal Mounting StructureSDR 07FDEA05030Valve · malfunctionedNR 2 FUEL TANK CROSS FEED WOULD NOT OPEN UP IN FLIGHT. ACN RELEASED FOR SERVICE. CLEANED AND RESEATED NR 2 FUEL CROSSFEED MAINIFOLD VALVE CONNECTOR PER SMP. TRANSFERED FUEL FROM NR 2 INTO 1&3 TANKS. PERFORMED TEST OF VALVE PER AMM 28-22-011-4. SYS CHECKS NORDec 11, 2007 · N237FE · Boeing 727247 · Aircraft Fuel Distribution SystemSDR 07FDEA04694Support · crackedTWO .250 CRACKS FOUND IN NOSE LANDING GEAR DOWN LOCK ACTUATOR SUPPORT ASSY. DURING SCHEDULED K CHECK INSPECTION. DAMAGE PART REPLACED.Oct 27, 2007 · N237FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 06FDEA2463Skin · corrodedFOUND FUSELAGE SKIN CORRODED UNDER STR 28-R BETWEEN FS 480 AND FS 500. DAMAGED WAS BLENDED AND FOUND TO BE OUT OF LIMITS IAW FEDEX B727 SRM 53-30-1. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW FEDEX B727 SRM 53-30-3 FIG 3. ALODINED AND PRIMED IAW FEDEXJul 6, 2006 · N237FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 06FDEA2462Stringer · corrodedFOUND STR 28-R AT FS 480 CORRODED; IN BILGE OF FWD PIT. FOUND DAMAGE TO STRINGER 28-R AT FS 480 OUT OF LIMITS. REMOVED AND REPAIRED STRINGER IAW FEDEX B727 SRM 53-10-3 FIG 1. ALODINED AND PRIMED IAW FEDEX B-727 SRM 51-10-2.Jul 6, 2006 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 05FDEA04143Window · brokenPDIS 237 56-10 0007743 04DEC05 FSD CLOSE R AT FL200, CAPT'S NR1 WINDSCREEN OUTER PANE CRACKED. TURNED CAPT'S WINDOW HEAT OFF AND COMPLIED WITH QRH PROCEDURE. FACT 04DEC05 23:58 FSD U REMOVED AND REPLACED L-1 WINDOW IAW AMM 56-11-011-4. ALSO REMOVED Dec 5, 2005 · N237FE · Boeing 727200 · Flight Compartment WindowsSDR 05FDEA02933Radar · malfunctionedRADAR INOP WITH RANGE AT 40 MILES, 15 LOW TILT, NO GND RETURN, LEVEL FLIGHT 80 MILE RANGE TILT 1.5 UP, RADAR SHOWED NUMEROUS RETURNS WITH VISUALLY NO WEATHER AHEAD. WEATHER RADAR OPS CHKS NORMAL ON GRND IAW 727-200AMM 34-41-000-0.Sep 15, 2005 · N237FE · Boeing 737247 · Weather Radar SystemSDR 04FDEA00375Bulkhead · corrodedCORROSION, AFT CARGO BAY, CORROSION ON 1183 BULKHEAD BS 1183 LBL 2 WL 153. *S/D* REMOVED BS 1183 BL 0 (I) BEAM. FABRICATED AND INSTALLED NEW (I) BEAM IAW FED EX EA 7-5310-70618 & SRM 51-30-2.Feb 9, 2004 · N237FE · Boeing 727200 · Fuselage Main, BulkheadSDR 04FDEA00245Stringer · corrodedCORROSION FWD CARGO BAY BS 685 STR 26R WL 145 ON STRINGER. LOCATED CORROSION FWD CARGO BAY BS 685 STR 26R WL 145 BLENDED CORRODED AREA (STR 26 RT) 4 INCHES LONG, BLEND OUT WAS OUT OF LIMITS. REPAIRED DAMAGED AREA, ALODINED & PRIMED IAW SRM 51-30-2, 5Jan 29, 2004 · N237FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA00238Frame · corrodedN00260 CORROSION (C53-113-01(2)), AFT CARGO BAY, FRAME HAS CORROSION BY FASTENER COLLAR AT BS 1050 LBL 19 WL 150 (FASTENER COMMON TO FLOOR TO SIDEWALL SUPPORT AND FRAME) BLENDED CORROSION ON FRAME AT BS 1050 LBL 19 WL 150 IN AN AREA OF 3X1X.013 O.TJan 28, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00239Angle · crackedANGLE CRACKED IN RT WHEEL WELL, FORWARD LOWER CORNER, AFT OF APU LOAD CONTROL VALVE. REMOVED ANGLE IN RT WHEEL WELL FWD LWR CORNER AFT OF APU LOAD CONTROL VALVE HOUSING. FABRICATED NEW ANGLE FROM BAC 1503-100058, 7075T6 LOT 509311. APPLIED PROTECTIVE TJan 28, 2004 · N237FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA00212Shear Tie · corrodedCORROSION (C53-113-01, 2) AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950F BETWEEN STR 29 LT AND 30 LT. CORROSION ON FRAME SHEAR TIE AT BS 950F BETWEEN STR 29 AND 30L IS OUT OF LIMITS PER SRM 51-10-1. FABRICATED A NEW SHEAR TIE AND REPLACED IT PER SRMJan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00209Frame · crackedAFT CARGO BAY, FRAME CRACKED AT FASTENER HOLE BS 1050 RBL 20 WL 149 (FLOOR TO SIDEWALL SUPPORT ATTACH FASTENER HOLE). REPAIRED AFT CARGO BAY FRAME AT BS 1050, RBL 20, WL 149 IAW FED EX E.A. 7-5310-55217.Jan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00208Frame · dentedAFT CARGO BAY, FRAME IS DENTED AT BS 1070 BETWEEN STRINGER 25 RT AND 27 RT. REPAIRED AFT CARGO BAY FRAME AT BS 1070 STR 25-27R IAW FED EX E.A. 7-5310-55218.Jan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA00210Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148. BLENDED CORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148 PER SRM 51-10-1. BLEND AREA WAS 2X1INCHES, ORIGINAL THICKNESS WAS .063. 100 PERCENT MATERIAL WAS REMOVED. REMOVED DAMAGED SHEAR TIE, BS 500, STJan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00207Shear Tie · corrodedCORROSION IN AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950D BETWEEN STRINGER 29 LT AND 28 LT. REMOVED CORROSION ON SHEAR TIE AT BS 900D BETWEEN STR 29L AND 28L. FABRICATED SHEAR TIE. ALODINE, PRIMED AND INSTALLED SHEAR TIE AT BS 350D BETWEEN STR 29L Jan 23, 2004 · N237FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA00203Frame · crackedCRACK AT NR 1 CARGO AFT FRAME BS 620, TWO INCHES INBOARD OF NR 1 DOOR STOP. REMOVED CRACK AT NR 1 CARGO AFT FRAME BS 620, TWO INCHES INBOARD OF NR 1 DOOR STOP AND REPAIRED PER 727 SRM 51-40-2.Jan 22, 2004 · N237FE · Boeing 727200 · Fuselage Main, FrameSDR 01FDEA00823Rib · corrodedRT HORIZ NR1 ELEVATOR HINGE RIB O/B LUG, O/B FACE HAS CORROSION (C55-391-20-3). REMOVED AND REPLACED PER EA 7-550-59272.Sep 7, 2001 · N237FE · Boeing 727247 · Elevator, Spar/RibSDR 01FDEA00772Fitting · crackedLT WHEEL WELL TIE STRAP AT BS 940-950 FITTING IS CRACKED AT STR 18A. REMOVED AND REPLACED TIE STRAP PER SRM 51-30-5, 51-30-2.Aug 28, 2001 · N237FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 01FDEA00747Splice · corrodedCORROSION AROUND FASTENERS BS 1177 WL 208 1 INCH I/B OF SKIN (UNDERSIDE). REMOVED AND REPLACED SPLICE ANGLE PER SRM 53-10-1, 51-30-1.Aug 20, 2001 · N237FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 01FDEA00746Stringer · corrodedCORROSION ON STR 26R BS 720E +10 TO 720D +11. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 1.Aug 20, 2001 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 01FDEA00751Crease Beam · corrodedCORROSION ON UNDERSIDE OF CREASE BEAM WEB BS 344 LBL 65 WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM 51-40-2 FIG 1.Aug 19, 2001 · N237FE · Boeing 727247 · Fuselage Main, StructureSDR 01FDEA00750Floorbeam · crackedTHREE CRACKED HOLES IN BS 344 FLOORBEAM WEB. *S/D* REMOVED AND REPLACED FLOORBEAM WEB PER SRM 51-40-2.Aug 19, 2001 · N237FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 01FDEA00749Stringer · corrodedCORROSION IN BOTTOM OF STR 27L BS 950E +16. REMOVED AND REPLACED STR PER SRM 53-10-1 FIG 1.Aug 18, 2001 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 01FDEA00748Stringer · corrodedCORROSION ON STR 27R BS 720F + 10 THROUGH 740 (FUSE 295). REMOVED AND REPLACED STRINGER.Aug 17, 2001 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 01FDEA00743Frame · dentedFOUR DENTS IN FRAME FLANGE AT BS 580 BET STR 22L - 25L. REMOVED AND REPLACED FRAME PER SRM 51-30-2.Aug 15, 2001 · N237FE · Boeing 727247 · Fuselage Main, FrameSDR 01FDEA00720Shear Tie · corrodedCORROSION ON FRAME SHEAR TIE BS 1130, WL 148, RBL 24. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-3, 51-20-1, 51-10-2.Aug 15, 2001 · N237FE · Boeing 727247 · Fuselage Main, StructureSDR 01FDEA00719Floorbeam · corrodedCORROSION (C53-111-01, 3) AROUND FASTENER HOLES LWR FLANGE OF 1070 FLOORBEAM BL 0 TO RBL 55. REMOVED AND REPLACED FLANGE PER SRM 53-10-8 FIG 8.Aug 15, 2001 · N237FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 01FEDA00745SkinN0901 CORROSION (TASK NO C53-132-01-1) ON EXTERNAL SKIN AROUND FASTENER HOLES FROM BS 700 - 720+10 STR 24R TO 27L (MARKED). S/D COMING *****Aug 15, 2001 · N237FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 01FDEA00724Web · crackedWEB CRACKED BS 344, LBL 12, WL 208. REMOVED AND REPLACED WEB PER EA 7-5310-59259.Aug 13, 2001 · N237FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 01FDEA00700Floorbeam · corrodedCORROSION ON LWR CHORD OF 1130 FLOORBEAM LWR FLANGE AROUND FASTENER HOLES LT SIDE TO RT SIDE. REMOVED AND REPLACED LOWER CHORD PER EA 7-5310-59239.Aug 13, 2001 · N237FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 01FDEA00694Skin · chafedEXTERIOR SKIN CHAFED AT BS 720D+12, STR 19L. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53-30-3 FIG 4.Aug 13, 2001 · N237FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 01FDEA00693Skin · chafedEXTERIOR SKIN CHAFED AT BS 720D+12" STR 19R. REMOVED AND REPLACED REPAIR DOUBLER PER 53-30-3 FIG 4.Aug 13, 2001 · N237FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 01FDEA00692Floorbeam · corrodedNR 877 CORROSION (C53-111-01(3)) ON LOWER FLANGE OF FLOORBEAM 1050 RBL 35, WL 202. ** S/D ** COMINGAug 13, 2001 · N237FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 01FDEA00723Frame · dentedFRAME DENTED BS 990 AT S 25L. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-59284.Aug 12, 2001 · N237FE · Boeing 727247 · Fuselage Main, FrameSDR 01FDEA00722Frame · dentedFRAME 970 DENTED BETWEEN S 25L AND S 26L. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-30-1.Aug 12, 2001 · N237FE · Boeing 727247 · Fuselage Main, FrameSDR 01FDEA00721Frame · dentedDENT IN FRAME FLANGE AT BS 560, STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-30-2.Aug 12, 2001 · N237FE · Boeing 727247 · Fuselage Main, FrameSDR 01FDEA00699Frame · dentedN 885 DENTS IN FRAME FLANGE AT BS 600 BETWEEN STR 23L AND 25L. ** S/D ** COMINGAug 12, 2001 · N237FE · Boeing 727247 · Fuselage Main, StructureSDR 01FDEA00744Skin · damagedWHILE WORKING CARD 7-5310-7-2301G2 PT 1 FOUND DAMAGED FASTENER HOLES. REPAIRED PER SRM 53-30-03 FIG 3A.Aug 11, 2001 · N237FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 01FDEA00701Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE BS 344, LBL 3-20, WL 208.Aug 10, 2001 · N237FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 00FDEA00792Gasper Fan · wornAFT T/O SMELL STRONG ELECTRICAL ODOR. USING LEFT NR 1 BLD, SWITCHED TO RIGHT PACK AND NR 3 BLD NO CHANGE. REMOVED AND REPLACED CIRCUIT BREAKER PNL LIGHT SOCKET.Nov 26, 2000 · N237FE · Boeing 727247 · Air Distribution FanSDR 00FDEA00788Detector · out of positionLOWER AFT BODY HEAT LIGHT CAME ON. REPOSITIONED AFT BODY OVERHEAT ELEMENT REF 26-14-001-2, 26-14-000-5, 30-13-000-5.Nov 24, 2000 · N237FE · Boeing 727247 · Overheat DetectionSDR 00FDEA00052Actuator · leakingAS FLAPS RETRACT AIR LIGHT FLICKERED ALONG WITH A SYS LOW PRESS LIGHT, THEN CAME ON STEADY. LOSS OF A SYS HYD LEFT NR 2 LEAD EDGE DEVICE FAIL. NR 2 KRUGER FLAP ACTUATOR LEAKING. *S/D* REMOVED AND REPLACED NR 2 LEAD EDGE ACT PER 727-200 MM 27-81-022-4.Feb 3, 2000 · N237FE · Boeing 727247 · Leading Edge Slat ActuatorSDR 99FDEA00493Unit · failedRT MLG IND UNSAFE ON EXTENSION. WHILE WORK CKLIST GEAR LATER WENT DOWN AND LOCKED IND FOR NO REASON. *S/D* REPLACED LAND GEAR ASSY BOX PRECAUTIONARY. OPER CK PER ENG AUTH 7-3209-4087-1 REVISION A AND MM 32-09-122-5 STEPS 5A-E.Dec 1, 1999 · N237FE · Boeing 727247 · Landing Gear Position and Warning
Back to N237FE, cancelled Dec 19, 2013