N136FE, cancelled Aug 6, 2012

Service difficulty reports · 25

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 = 'N136FE' AND deregistration_id = 'N136FE-2012-08-06'
  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 05FDEA03795Light · inoperativeRTO FOR AFT AIRSTAIR LIGHT IAS 75 KTS. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22NOV05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. VERIFIED AFT AIRSTAIR IS CLOSED AND RED LIGHT EXTINGUISHED. COMPLIED WITH TRO HIGH ENENov 14, 2005 · N136FE · Boeing 727100 · Door Warning SystemSDR 05FDEA03509Door · openAFTER DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE. RAN QRH AND NO SUCCESS. APPLIED SYSTEMS KNOWLEDGE AND COULD NOT SOLVE PROBLEM. RETURNED TO MEMPHIS. AFTER BLOCK-IN TO MEMPHIS, AND A VISUAL INSPECTION, FOUND AFT CARGO DOOR OPEN, AND FAIRING DOOR CLOSED. SUSOct 26, 2005 · N136FE · Boeing 72725C · Cargo/Baggage DoorsSDR 05FDEA02661Bracket · crackedCOVE PANEL BRACKET IS BROKEN ON LOWER WING PANEL BELOW NR 3 SPOILER. REMOVED AND REPLACED 3 EA BRACKET P/N 65-21658Y29, 65-21658-27, AND 65-21658Y30, AND 1 EA ROD P/N 69-17911-18 IAW SRM 51-30-2.Aug 25, 2005 · N136FE · Boeing 727100 · Wing, Attach FittingsSDR 03FDEA01982Battery · dischargedFWD ENTRY AND COCKPIT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES FOR OVERHEAD LIGHT ASSY'S PER FEDEX MM 33-50-101-2. CHECKS GOOD PER FEDEX MM 33-50-101-2.Nov 25, 2003 · N136FE · Boeing 727100 · Emergency LightingSDR 03FDEA01917Frame · crackedFOUND CRACK ON FRAME TOOLING HOLE BS 1050 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1050, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.Nov 14, 2003 · N136FE · Boeing 727100 · Fuselage Main, FrameSDR 03FDEA01916Frame · crackedFOUND FRAME CRACKED AROUND OPEN HOLE BS 1070 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1070, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 & FED EX EA 7-5310-55117.Nov 14, 2003 · N136FE · Boeing 727100 · Fuselage Main, FrameSDR 03FDEA01912Web · corrodedCORROSION ON AFT RIGHT WEB AT BS 1130, RBL 61, WL 208. CORROSION ON AFT RIGHT WEB BS 1130, RBL 61, WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED WEB IAW SRM 51-40-2.Nov 13, 2003 · N136FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 03FDEA01911Web · corrodedCORROSION (C53-224-04), SHEAR WEB BS 1166-1173, RBL 53-62, WL 208.Nov 13, 2003 · N136FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 03FDEA01907Beam · corrodedCORRODED LONGITUDINAL BEAM BS 846, LBL 44, WL 208.Nov 12, 2003 · N136FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 03FDEA01890Skin · bulgedEXTERNAL SKIN BULGED AT BS 350 BETWEEN STR 25R AND 26R. INVESTIGATED BULGED SKIN BS 350, STR 25R & 26R. FOUND SKIN TO BE CORRODED BETWEEN SHIM AND SHEAR TIE. REMOVED OLD SHIM. FABRICATED NEW SHIM. ALODINED, PRIMED, AND INSTALLED. ALL PER SRM 51-30-2, MMNov 7, 2003 · N136FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 03FDEA01889Skin · damagedLWR AFT CARGO DOOR SKIN, SKIN DAMAGED ALONG FWD EDGE AT NR 2 STOP FITTING FROM TOP. *S/D* INSPECTED LWR AFT CARGO DOOR SKIN ALONG WD EDGE, DAMAGE WAS 1 X 16 X .25 INCH FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLENov 7, 2003 · N136FE · Boeing 727100 · Cargo/Baggage DoorsSDR 03FDEA01891Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 RBL 61 WL 208. *S/D* REMOVED CORROSION FROM UPPER CHORD BS 1130 FLOORBEAM, RBL 61, WL 208 AND FOUND OUT OF LIMITS. REMOVED CORRODED SECTION OF BEAM. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS. ALL WORKNov 7, 2003 · N136FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 03FDEA01404Panel · malfunctionedON INITIAL GEAR EXTENTION, ALL RED GEAR DOOR LIGHTS OPERATED NORMALLY BUT ONLY GREEN MAIN GEAR LIGHTS ILLUMINATED (NO GREEN NOSE GEAR LIGHT). RECYCLED GEAR UP / DOWN, TWO MAIN INDICATED BRIGHT GREEN, NOSE INDICATED VERY DIM GREEN, CYCLED LIGHT TEST SWITCH ANDSep 3, 2003 · N136FE · Boeing 727100 · Landing Gear Position and WarningSDR 02FDEA00867Handle · out of positionON DEPARTURE, FWD CARGO DOOR LT ILLUM FOLLOWED RED TABS AND ELECTED TO RETURN TO PIT FOR MX ACTION. PRESSURIZATION NOT NORMAL/NOTED PRESS BUMP DURING CLIMBOUT. UPON INSPECTION OF FORWARD LOWER CARGO DOOR. FOUND HANDLE INSIDE DOOR SLIGHTLY OPPOSITE OF OUTSIDNov 19, 2002 · N136FE · Boeing 727100 · Cargo/Baggage DoorsSDR 01FDEA00830Duct · crackedPASSING 1500 FT ABOVE GROUND LEVEL NR 3 ENG FIRE LIGHT ILLUM WHEN THROTTLE RETARD. REMOVED AND REPLACED 8TH STAGE BLEED DUCT PER MM 36-00-001-2.Sep 11, 2001 · N136FE · Boeing 72725C · Pneumatic Distribution SystemSDR 00FDEA00807Connector · failed00-331 ON DEPARTURE, NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. ** S/D ** ACCOMPLISH WIND MILL INSP DUE TO ENG SHUT DOWN PER MM 72-00-518D. R&R BYPASS SWITCH AS PER 727-100 MM 79-33-002-4. OPS TEST NORMAL.Nov 29, 2000 · N136FE · Boeing 72725C · Engine Oil QuantitySDR 99FDEA00007Retract Mech · malfunctioned99-0007 - DURING FLAP RETRACT, NR 6 SLAT DID NOT FULLY RETRACT. UNABLE TO CORRECT WITH RED TAB PROC. INSPECT SLAT, NO DEFECT FOUND. RAN NR 1 ENG WITH HYD PRESS, EXTEND AND RETRACT ALL LEAD EDGE DEVICE WITH NO FAULT OR PROBLEM FND. MOCC NOTIFIED, AC OK FOR Jan 9, 1999 · N136FE · Boeing 72725C · Leading Edge Slat Control SystemSDR 98FDEA00372Gpws · malfunction98-0141 - GPWS WARNING FOR GEAR AT 500 FT ABOVE GROUND LEVEL (FULL LANDING CONFIGURATION). DURING TROUBLE SHOOTING PROCESS, FOUND TAILSKID CANNON PLUG. INSTALLED GEAR PINS AND CYCLED GEAR AND FLAPS SEVERAL TIMES. ALL INDICATIONS WERE NORMAL. GPWS CHECKED NMay 29, 1998 · N136FE · Boeing 72725C · Ground Proximity SystemSDR 96FDEA01421Stick Shaker · failed testCONTINUOUS STICK SHAKER AT TAKEOFF. STANDARD POWER TAKEOFF 36C, ADVANCED THROTTLES TO MOMENTARY FIREWALL POWER. PULLED AC NR 1 STALL WARNING CIRCUIT BREAKER, SHAKER STOPPED. ATTEMPTED 1 RESET OF CIRCUIT BREAKER, STILL HAD SHAKER. PULLED CIRCUIT BREAKER ANDAug 30, 1996 · N136FE · Boeing 72725 · Airspeed/Mach IndicatorSDR 96FDEA01369Return Hyd Line · brokenTOTAL LOSS OF A-SYS HYD AT FLT LEVEL 280. GEAR MANUALLY EXTENDED AND FLAPS WERE EXTENDED THROUGH ALTERNATE FLAP MASTER. REMOVED AND REPLACED SPOILER RETURN LINE RT. FOUND 2 BROKEN BRACKETS AT SPOILER CLOSE OUT PANEL, REMOVED AND REPLACED SAME (P/N 65-21658-Aug 15, 1996 · N136FE · Boeing 72725C · Drag Control SystemSDR 96FDEA01050Floor Web · corrosionCABIN CORROSION ON FLOOR WEB STA 1178 APPROX 55 INCHES LBL UPPER SURFACE UNDER CHORD ANGLE. CUT OUT DAMAGED FLOOR WEB AREA, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2.May 28, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01049Vert Angle · crackedVERT ANGLE CRACKED AT LIGHTENING HOLE AT BS 1183 RBL 26 TO 9 WL 253. PERFORMED 1183 VERTICAL BEAM MOD PER BOEING SERVICE BULLETIN 727-53-0182 PG 23 SRM 53-10-9.May 28, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01048Hinge Casting · brokenLARGE HINGE ASSEMBLY FOR LEFT HAND O/B AILERON HAS BAR BROKEN OFF. REMOVED HINGE CASTING AND INSTALLED A SERVICEABLE CASTING PER DRAWING NR 65-19260 SHEET 1.May 28, 1996 · N136FE · Boeing 72725C · AileronsSDR 96FDEA01047Door Frame · crackedCRACK IN LWR FWD CORNER OF DOOR FRAME OF FWD LWR CARGO APPROX 1 INCH LONG. STOP DRILLED CRACK AND INSTALLED 7075-6, 0.90 DOUBLER ANGLE PER SRM 53-10-4 PG 39 TO 41.Apr 30, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01510Hyd Line · brokenDURING CRUISE FL 290, A/C LOST SYS A-HYD, NO APPARENT REASON. FOUND NR 2 SPOILER PRESS LINE BROKE. REMOVED AND REPLACED PRESS LINE, REMOVED CASE DRAIN FILTERS AND PRESS FILTERS, NO CONTAMINATION FOUND. INSTALLED NEW CASE DRAIN FILTERS PER MM 29-11-41, PRESSOct 7, 1995 · N136FE · Boeing 72725C · Hydraulic System, Main
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