Boeing 727-200

Service difficulty reports · 2,835

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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"

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SDR 03FDEA00996Tripler · wornMDIS 463 53-30 0005660 25JUN03 BFM CLOSER COMPLY WITH EA 7-5330-70962; MAIN CARGO DOOR TRIPLER WEAR. FACT 27JUN03 13:59 BFM R COMPLIED WITH EA NR 7-5330-70962, FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR, P/N 53FX1301-7/-9.Jun 28, 2003 · N463FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00990Skin · damagedWHILE WORKING FOUND AREA OF OIL CANNING ON FWD CARGO DOOR LOWER SKIN 10 INCHES FROM FRONT. REPAIRED FWD CARGO DOOR LOWER SKIN IAW SRM 52-00-3 FIG 3.Jun 27, 2003 · N216FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00974Engine · malfunctionedAT FL330, NR 2 ENGINE OIL TEMP ROSE TO HIGH IN THE YELLOW RANGE. ADDING FUEL FLOW BY INCREASING THROTTLE DID NOT HELP. AFTER 15 MINS IN YELLOW BAND, SHUTDOWN NR 2 ENGINE IAW ENGINE FAILURE/SHUTDOWN CHECKLIST. WHEN THROTTLE RETARDED TO IDLE, NR 2 ENG OIL Jun 26, 2003 · N236FE · Boeing 727200 · Engine Oil Indicating SystemSDR 03FDEA00971Floorbeam · chafedBS 740 FLOORBEAM IS CHAFED IN AREAS FROM LBL-45 RBL 45 WL 208. REPAIRED FLOORBEAM IAW EA 7-5310-54878.Jun 25, 2003 · N216FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00952Frame · crackedCRACKED FRAME SHEAR TIE STA 540 ABOVE STR 18L. REPAIRED SHEAR TIE BS 540 ABOVE STR 18L IAW SRM 51-40-3.Jun 23, 2003 · N216FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00953Shear Tie · crackedN00460 CRACKED FRAME SHEAR TIE STA 580 ABOVE 18L ** SD ** COMINGJun 23, 2003 · N216FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00954Shear Tie · crackedN00461 SHEAR TIE CRACKED BS 560 ABOVE STR 18L. ** S/D ** COMINGJun 23, 2003 · N216FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00955Shear Tie · crackedN00459 CRACKED FRAME SHEAR TIE AT STA 500 ABOVE STR 18 LT. ** SD ** COMINGJun 23, 2003 · N216FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00938Frame · crackedCRACKED FRAME SHEAR TIE STA 580 ABOVE STR 18L. REPAIRED SHEAR TIE CLIP AT BS 580 ABOVE 18L PER SRM 51-40-3.Jun 20, 2003 · N216FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00937Frame · corrodedCORROSION AFT CARGO BAY STA 950D STR 29 LT SHEAR TIE HAS CORROSION. REPAIRED SHEAR TIE AT BS 950D STR 29 LT IAW FED EX EA 7-5310-54855.Jun 20, 2003 · N487FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00936Keelbeam · corrodedN00389 CORROSION AFT CARGO BAY, STA 950C TO 950F STR 29L HAS CORROSION. REPAIRED LT KEEL BEAM STR 29L IAW FED EX E.A. 7-5310-54856.Jun 20, 2003 · N487FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA00907Frame · dentedN00368 970 FRAME DENTED AT S25L. REPAIRED FRAME AT BS 970 STR 25L IAW SRM 51-40-3, FIG 1, BS 970 FRAME DENT AT STR 25L OUT OF LIMITS IAW SRM 53-10-1.Jun 18, 2003 · N216FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00908Frame · gougedN00369 990 FRAME GOUGED BETWEEN S25L - S26L. REPAIRED FRAME AT BS 990 BETWEEN STR 25L - STR 26L PER SRM 51-40-3 FIG 1, BS 990 FRAME GOUGE OUT OF LIMITS IAW SRM 53-10-1 AT STR 25L - STR 26L.Jun 18, 2003 · N216FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00906Frame · dentedN00367 950F FRAME DENTED BETWEEN S26L AND S25L. REPAIRED FRAME AT BS 950F BETWEEN STR 26L AND STR 25L IAW SRM 51-40-3 FIG 1, BS 950F FRAME DENT BETWEEN STR 25L AND STR 26L OUT OF LIMITS IAW SRM 53-10-1.Jun 18, 2003 · N216FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00903Shear Tie · corrodedN00586 CORROSION (C53-113-01) FWD CARGO STA 720B LBL 2 ON FRAME SHEAR TIE. CORROSION ON FWD CARGO STA 720B, LBL 2, SHEAR TIE WAS FOUND OUT OF LIMITS. REMOVED AND REPAIRED ACTUATOR PANEL AND SPLITER TO ACCESS. REMOVED DAMAGED SHEAR TIE. FABRICAJun 18, 2003 · N492FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00905Frame · crackedN00801 FRAME AT BS 640, LBL 3, WL 155 IS CRACKED ON UPPER FLANGE IN RADIUS. CUTOUT CRACKED PORTION OF FRAME IN AREA OF 2.2 INCHES X 1.8 INCHES. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON FRAME BS 640, LBL 3, W/L 155 IAW SRM 51-40-3 FJun 18, 2003 · N492FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00904Stiffener · corrodedN00606 CORROSION (C53-132-02-1) ON UPR SURFACE HORIZONTAL FLANGE BS 744, LBL 8, WL 159 ABOVE DELTA BEAM FWD OF PANEL 3209L IN AIR CONDITIONING BEAY. REMOVED CORROSION AREA 3 INCHES X 1 INCH X .021 INCH FROM ORIGINAL .100 INCH FOUND OUT OF LIMITS IAW SJun 18, 2003 · N492FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00899Smoke Detector · malfunctionedON T/O CPR PASSING 3000 AGL NR 4 UPPER DECK SMOKE DETECTOR LIGHT ILLUMINATED, MASTER FIRE LIGHT ON GLARESHIELD ILLUMINATED. FIRE WARNING BELL SOUNDED, DOWN LOADED CARGO. CHECKED CARGO FOR DEFECTS, FOUND NO DEFECTS. PRECAUTIONARY CHANGED NR 4 SMOKE DETECTJun 17, 2003 · N212FE · Boeing 727200 · Smoke DetectionSDR 03FDEA00882Stringer · corrodedCORROSION (C53-113-01) FWD CARGO STA 660, RBL 6 IN STR 28R. REMOVED CORROSION AND REPAIRED STR 28 RT AT BS 660 PER SRM 53-10-1, 53-10-3, FIG 1.Jun 16, 2003 · N492FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00885Skin · dentedFUSELAGE SKIN HAS A DENT, STRINGER 6L, BS 720C. REPAIR DENTED SKIN PER SRM 53-30-3 FIG 3.Jun 16, 2003 · N273FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2003749007Sensor · will not testLOWER AFT BODY OVERHEAT WILL NOT TEST. DEFERRED PER MEL 26-10-2. SP 26-10-2 COMPLIED WITH. DMI 13274 PLACARD INSTALLED. MAINTENANCE CONTROL NOTIFIED. REF DMI 13274; LOWER AFT BODY OVERHEAT WILL NOT TEST. TROUBLESHOT AND TESTED SYSTEM IAW BMM 26-14-00. NJun 16, 2003 · N749DH · Boeing 727200 · Overheat DetectionSDR 03FDEA00886Skin · corrodedCORROSION (C53-113-01, 2) BULGING SKIN ON STR 28L, BS 1055.Jun 16, 2003 · N273FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00884Skin · corrodedCORROSION ON INTERIOR SIDE OF SKIN AT BS 664, RBL 4 TO LBL 4.Jun 16, 2003 · N492FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00883Stringer · corrodedCORROSION (C53-100-01) IN RT MLG WHEEL WELL ON UPPER SURFACE OF STRINGER 18A SHELF FROM BS 900 TO BS 940.Jun 16, 2003 · N492FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00881Shear Tie · corrodedCORROSION (C53-113-01) STA 660, LBL 4 - RBL 4 ON FRAME SHEAR TIE.Jun 16, 2003 · N492FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00880Shear Tie · corrodedCORROSION (C53-113-01) FWD CARGO STA 640, RBL 4 - LBL 4 OF FRAME SHEAR TIE.Jun 16, 2003 · N492FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00879Floorbeam · corrodedCORROSION (C53-224-06) TOP OF FLOORBEAM BS 328, LBL 40, WL 208.Jun 16, 2003 · N492FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00877Skin · lightning strikeEXTERIOR SKIN, LIGHTNING STRIKE BS 355, .5 INCH BELOW STRINGER 21 LT.Jun 16, 2003 · N487FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00872Warning System · activatedAFTER TAKEOFF AND PLACING THE GEAR LEVER TO UP RECEIVED A RED DOORS LIGHT. RECYCLED GEAR AND LIGHT WENT OUT. UNABLE TO DETERMINE WHICH DOOR CAUSED RED LIGHT TO ILLUMINATE. NO MENTION OF AMBER LIGHT ON S/O ANNUN PANEL. PERFORMED ADJ/TEST PER AMM 32-62-011-5Jun 13, 2003 · N270FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA00869Transformer · failedON THE 20-40 MILE RANGE THE FAIL MESSAGE APPEARS WITH NO RETURNS. AT THE 80 MILE RANGE IT WOULD WORK INTERMITTENLY. REMOVED AND REPLACED WX RADAR R/T IAW 727 M/M 34-41-041-4. OK FOR SERVICE.Jun 13, 2003 · N236FE · Boeing 727200 · Weather Radar SystemSDR 03FDEA00866Warning Light · illuminatedAMBER AFT STAIR LIGHT ILLUMINATED AFTER TAKEOFF, EXTINGUISHED AFTER LANDING. RAN RED TAB CHECKLIST AND TALKED TO GOCC LANDING OK. MEL 12JUN03 09:42 MEM U ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22JUN03 MEL 52-06-B: AMBER AJun 12, 2003 · N484FE · Boeing 727200 · Entrance StairsSDR 03FDEA00863Skin · crackedFWD ENTRY DOOR FWD UPPER CORNER OF DOOR SKIN IS CRACKED JUST BELOW UPPER GATE. REPAIRED FWD ENTRY DOOR, AFT UPPER CORNER OF DOOR SKIN, IAW SRM 52-00-2, 52-00-3, FIG 4.Jun 6, 2003 · N487FE · Boeing 727200 · Passenger/Crew DoorsSDR 03FDEA00862Angle · corrodedCORROSION (C53-111-02) ON FWD CARGO DOOR LOWER BEAM ANGLE 27 INCHES AFT OF FWD EDGE 1.5 INCH UP FROM BOTTOM EDGE. REMOVED CORROSION ON FWD CARGO DOOR LOWER BEAM ANGLE AND T-ANGLE AT FWD EDGE AT 27 INCHES. FOUND TO BE OUT OF LIMITS. LOCATED HOLES ON NEW T-Jun 6, 2003 · N487FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA00861Angle · corrodedWHILE WORKING CARD 00357 (DOOR 6030) DISCOVERED A CORROSION ON LOWER BEAM ANGLE WEB 45 INCHES AFT OF FWD EDGE 1.5 INCHES UP FROM BOTTOM EDGE ON NR 1 CARGO DOOR. REMOVED CORROSION ON LOWER BEAM ANGLE WEB 45 INCHES AFT OF FWD EDGE, FOUND TO BE OUT OF LIMITS. Jun 6, 2003 · N487FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00860Frame · corrodedCORROSION (C53-113-01), ON FRAME BS 950D STR 29R. CUT OUT AND REMOVED DAMAGED AREA OF FRAME. FABRICATED AND INSTALLED REPAIR BS 950D, STR 29R IAW SRM 53-10-4, FIG 15.Jun 6, 2003 · N487FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00850Stringer · corrodedCORROSION (C53-113-01,1) IN STR 27L BS 720F + 13 STR 27L BS 720F + 13 FOUND TO BE OUT OF LIMITS. REMOVED STR 27L FROM 720E + 10 TO 720F + 18. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS, ALL WORK DONE IAW SRM 53-10-3. REINSTALLED GASPER AIR FAN, REMOJun 3, 2003 · N498FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA00849Shear Tie · corrodedCORROSION (C53-113-01(17) SHEAR TIE BS 560 BETWEEN STR 26-27L. CORROSION ON SHEAR TIE IN A .75 X .75 INCH AREA FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-1, 51-30-2, 51-10-2.Jun 3, 2003 · N498FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00852Keelbeam · corrodedLOWER WEB OF DELTA KEEL BEAM HAS CORROSION ON UPPER SURFACE AROUND SUPPORT STRUCTURE AND LOWER SURFACE AROUND FASTENER HEADS, BS 740-870. REMOVED AND REPLACED LOWER WEB OF DELTA KEEL BEAM BS 740 TO BS 870 RBL 5 TO LBL 5 PER SRM 51-20-1.Jun 3, 2003 · N498FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA00851Shear Tie · corrodedCORROSION (C53-113-01,2) ON SHEAR TIE BS 950B, LBL 8-10, WL 140. REMOVED CORROSION ON SHEAR TIE BS 950B LBL 8-10 WL 140 AREA .65 X 5.00 X .013 INCH DEEP FROM ORIGINAL .071 FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED SHEAR TIE PER SRM 53-10-4.Jun 3, 2003 · N498FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00841Hinge · damagedMDIS 245 53-30 0005255 27MAY03 BFM CLOSE R COMPLY WITH E.A. NR 7-5330-70910 FUSELAGE - MAIN CARGO-RE WORK OF ATTACHMENT HOLE (AD 2002-16-19). FACT 30 MAY 03 15:18 BFM R COMPLIED WITH E.A. 7-5330-70910 - FUSELAGE - MAIN CARGO - REWORK OF HINGE ATJun 1, 2003 · N245FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR XNOA01124Brake Assy · unknownAFTER RELEASING BRAKES; ON POWER OUT OF MCO HEARD LOUD POP AND WHEN APPLYING PRESSURE TO BRAKES FELT VIBRATION COMING FROM MLG AREA. JACKED EACH MLG, INSPECTED EACH BRAKE & CYCLED NUMEROUS TIMES. NO DEFECTS NOTED. SERVICED ALL BRAKE LOCKOUTS. BRAKES CHECKEMay 31, 2003 · N76753 · Boeing 727200 · Landing Gear Brake SystemSDR 03FDEA00827Accessory Unit · false indicationDURING T/O GEAR RETRACTION, RED "RIGHT GEAR" LIGHT REMAINED ILLUMINATED. FOLLOWED RED TAB PROCEDURES BUT LIGHT REMAINED ON. NO OTHER LIGHTS OR INDICATIONS OBSERVED. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND OPS CHECKED GOOD IAW M/M 32-09-122May 30, 2003 · N496FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA00823Sensor · inoperativeON TAKE OFF, LANDING GEAR LEVER WOULD NOT RETRACT PAST THE OFF DETENT. PERFORMED QRH PROCEDURE FOR LANDING GEAR LEVER LATCH FAILED TO RELEASE. T/S PER 727-200 WDM 32-31-01. OHM CHECKED ENTIRE AIR & GROUND SENSOR CIRCUITS FROM L/G ACCESSORY RACK PLUG ANDMay 28, 2003 · N467FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA00818Skin · crackedEXT SKIN IS CRACKED AND BULGED OUTWARD AT BS 700, STR 27 LT. REPAIRED DAMAGED SECTION OF SKIN BS 688 TO BS 714 STR 26 LT PER SRM 53-30-3 FIG 5 AND FED EX EA 7-5330-70412. REMOVED AND REPLACED SHEAR TIE PER SRM 51-20-1, 51-10-2.May 27, 2003 · N498FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00817Channel · corrodedCORROSION LT WHEEL WELL BS 927-932 LBL 65 WL 188 STR 18A SHELF. REMOVED AND REPLACE SILL CHANNEL BS 870-936, WL 188, LBL 65 AT STR 18A PER SRM 51- 30-2, 51-30-5.May 27, 2003 · N490FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA00739Warning Light · illuminatedPASSING FL230, 330 KIAS, EPR 2.01/2.07/2.01, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. LEVELED OFF AT FL 260 AND PRIOR TO COMPLETING RED TABS , LOWER AFT BODY OVERHEAT LIGHT EXTINGGUISHED. RED TABS COMPLETED AND SYSTEM TEST GOOD. AT LEVEL OFF FL260 THROMay 16, 2003 · N269FE · Boeing 727200 · Overheat DetectionSDR 03FDEA00732Tripler · wornCOMPLY WITH E.A. 7-5330-70385 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR. FACT 15MAY03 21:19 BFM U COMPLIED WITH E.A. 7-5330-70385 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR.May 15, 2003 · N258FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00731Channel · corrodedLT WHEEL WELL HAS CORROSION AT STRINGER 18A CHANNEL BS 939 & 912 UPR SURFACE. REMOVED AND REPLACED SILL CHANNEL BS 870-940, LBL 65, WL 190 AT STR 18A PER SRM 51- 30-5, 51-30-2.May 14, 2003 · N485FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00730Pin · vibratesAFTER LANDING, LESS THAN 80 KNOTS, NOSE WHEEL BEGAN SEVERE VIBRATIONS. SHUT DOWN ON THE RUNWAY. REPLACED NOSE GEAR LINK PIN. OP CHECKS NORMAL PER B727-200 MM 32-21-021-6. OK FOR SERVICE.May 14, 2003 · N268FE · Boeing 727200 · Nose/Tail Landing GearSDR 03FDEA00704Tripler · wornMAIN CARGO DOOR TRIPLER WEAR. COMPLIED WITH EA 7-5330-70376 BLENDED AREA, EDDY CURRENT INSP, NO CRACKS NOTED. OK FOR SERVICE.May 9, 2003 · N269FE · Boeing 727200 · Fuselage Main, Plate/Skin
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