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 SCNA01707Warning System · activatedENGINE FAILURE INDICATION ON TAKEOFF. NR 3 GENERATOR BREAKER TRIP AND AUTO PACK TRIP OFF LEFT AND RIGHT PACK. PLACED ON MEL.Aug 9, 2001 · N211DB · Boeing 727200 · Engine Indicating SystemSDR AALA20011511Line · leakingDFW - FLT 1744 - EN ROUTE DFW-DTW - AIR INTERRUPTED WITH HYDRAULIC SYSTEM 'A' LOSS OF QUANTITY AND PRESSURE. RETURNED TO DFW LANDED WITHOUT INCIDENT. REPLACED LEFT ELEVATOR PACK HYDRAULIC LINE. SERVICED SYSTEM. LEAK AND OPERATIONAL CHECK OK. SYSTEM GROUNDJul 20, 2001 · N706AA · Boeing 727200 · Hydraulic Power SystemSDR EISA20010103Light · inoperativeEMERGENCY LIGHT OUT L1 DOOR, OPERATES DIMLY. REMOVED AND REPLACED LIGHT ASSY IAW MM 33. OPS CHECK GOOD.Jun 28, 2001 · N702NE · Boeing 727200 · Emergency LightingSDR EISA20010093Wire · brokenNOSE GEAR UNSAFE LIGHT ON WITH LANDIN GEAR DOWN RECYCLED GEAR TO EXTINGUISH LIGHT.CORRECTIVE ACTION:REPAIRED NOSE LANDING GEAR DOWN LOCK SWITCH WIRES BY SPLICING IAW B727 STANDARD WIRING MANUAL 20-30-22. OPS CHECKS GOOD IAW B727 32-61-71.Jun 13, 2001 · N702NE · Boeing 727200 · Landing Gear System WiringSDR C8GA20010015Engine · out of adjFLT 713 FROM JAX TO MCO. DURING THE TAKEOFF ROLL, THE NR 3 ENGINE EGT WENT TO RED LINE 630 DEGREES, THROTTLE PULLED BACK NOT TO EXCEED EGT PARAMETERS. AIR TURNBACK TO JAX AND LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUN AND ADJUSTED EGT ON NR 3 ENGINE AND Jun 11, 2001 · N713AA · Boeing 727200 · Engine (Turbine/Turboprop)SDR AALA20010803Wire · brokenDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEN FIRST CLASS AND COACH CLASS BROKEN. REPLACED EMERGENCY EXIT LIGHT WIRE BETWEEN FIRST CLASS AND COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Apr 18, 2001 · N894AA · Boeing 727200 · Emergency LightingSDR DHL2001747508Frame · damagedD-CHECK, REMOVE EXISTING REPAIR AT STA 950 STR 28R ON 950 CHORD BETWEEN STR 28-26R TO VERIFY IF REPAIR LEGAL WITH ANY DATA THEN INSTALL APPROVED REPAIR. FABBED, LOCATED, DRILLED AND DEBURRED FILLER & TRIPPLER IAW 727 SRM 51-30-5.Apr 17, 2001 · N747DH · Boeing 727200 · Fuselage Main, FrameSDR AALA20010769Light · inoperativeBNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Apr 10, 2001 · N894AA · Boeing 727200 · Emergency LightingSDR DHL2001747502Frame · crackedD-CHECK - THE STA 360 FRAME AT STR L IS CRACKED. CUT OUT DAMAGE IN FRAME PER HAC DWG 2950 AND FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED DOUBLERS, FILLER AND STRINGER CLIP PER HAC DWG 2950 AND 727 SRM 51-30-2 PG 14-14A. COMPLETED IAW EO 22253-01-002. Apr 5, 2001 · N747DH · Boeing 727200 · Fuselage Main, FrameSDR DHL2001747501Angle · crackedD-CHECK - FWD CARGO STA 480, FS 560 - S26R ANGLE CRACKED. REMOVED CRACKED ANGLE PER SRM 51-30-2. FABRICATED NEW ANGLE FROM 7075 T6 0.050 PER SRM 51-10-5 & ORIGINAL. TREATED PER SRM 51-10-2 AND PRIMED PER 51-20-11. INSTALLED ANGLE PER SRM 51-30-2. (REF N/RApr 2, 2001 · N747DH · Boeing 727200 · Fuselage Miscellaneous StructureSDR DHL2001747500Spar · corrodedD-CHECK, LEFT OTBD T/E MID FLAP, MID SPAR HAS CORROSION NEAR INBD END CLOSE OUT R/O. CORROSION BEYOND LIMITS PER SRM 57-50-2 (EXFOLIATED). REPAIR PER B727 SRM 51-40-4 FIG 1. REMOVED DAMAGED SECTION OF 'T' EXTRUSION PER 51-40-4 & 51-30-2. MATERIAL 2024-0 O.Apr 1, 2001 · N747DH · Boeing 727200 · Trailing Edge FlapsSDR DHL2001747522Seat Track · damagedD-CHECK, SEAT TRACK SECTION STA 680-520 RBL 22.45 HAS SURFACE CORROSION. TWO LUGS DAMAGED OUT OF LIMITS AT STA 530. FOUND DEEP GOUGE IN TRACK OUT OF LIMITS.Mar 22, 2001 · N747DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001747504Skin · damagedD-CHECK - REMOVED AND REPLACED EXISTING REPAIR AT BS 1223 S26R. REPAIR PER SRM 53-30-3. REMOVED EXISTING REPAIR AT STA 1223 S26R IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-303 FIG 25.Mar 21, 2001 · N747DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2001747507Floorbeam · crackedD-CHECK, FWD CARGO PIT ST 580 S 27L, FLOORBEAM CRACKED. REMOVED CRACKED AND DAMAGED PORTION OF Z-ANGLE IAW 51-10-04 FIG 4 PER SRM. ALODINED PER SRM 51-10-2. PRIMED PER SRM SOPM 20-41-02. INSTALLED PARTS PER SRM 53-10-5 FIG 4 SHEET 2 AND FASTENERS IAW SRM 51Mar 21, 2001 · N747DH · Boeing 727200 · Fuselage Main, Floor BeamSDR DHL2001747503Skin · damagedD-CHECK - REMOVED AND REPLACED EXISTING REPAIR AT BS 1223 S26L. REPAIR PER SRM 53-30-3. FABRICATED AND LOCATED NEW REPAIR DOUBLER .HFEC IND NO CRACKS OR CORROSION FOUND. TREATED PARTS PER SRM 51-10-2 PG 3-4 AND PRIMED PER SOPM 20-41-02. INSTALLED PER SRM 53Mar 21, 2001 · N747DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR DHL2001747506Structure · corrodedD-CHECK, CORROSION ON LT AFT LAV FLOOR JUST INBD OF FRAME 1166 LT. REPAIR PER SRM REMOVED AND REPLACED MOP SILL. REMOVED DAMAGED AREA PER 727 SRM 51-40-2. ALODINED PARTS PER 727 SRM 51-10-2. PRIMED REPAIR PARTS PER SOPM 20-41-2. INSTALLED REPAIR PARTS (-2,Mar 20, 2001 · N747DH · Boeing 727200 · Fuselage Miscellaneous StructureSDR DHL2001747505Web · corrodedD-CHECK - CORROSION JUST INBD OF RT AFT LAV DUMP HOLE IN FLOOR JUST FWD OF STA 1183. CUT OUT DAMAGED AREA AT FLOOR WEB PER B727 SRM 51-40-2 PG 1-6. FABRICATED AND LOCATED HOLES IN DOUBLER PLATE AND FILLER PER B727 SRM 51-40-2 PG 1-6. ALODINED PER SRM 51-10-2Mar 20, 2001 · N747DH · Boeing 727200 · Fuselage Miscellaneous StructureSDR DHL2001747509Floorbeam · corrodedD-CHECK, TOP CAP OF FLOORBEAM FS 400 RBL 18 HAS EXFOLIATED CORROSION ON BOTTOM-SIDE AT FLOORBOARD SCREW HOLE. ALODINED PER B727 SRM 51-10-2 PG 1. FABRICATED ANGLES -2 & -3 AND LOCATED HOLES PER B727 SRM 53-10-8 PG 44-48. ALODINED PER B727 SRM 51-10-2 PG 1. Mar 13, 2001 · N747DH · Boeing 727200 · Fuselage Main, Floor BeamSDR DHL2001747515Seat Track · corrodedD-CHECK - SEAT TRACK SECTION STA 970-870 HAS AREAS OF LIGHT CORROSION RBL 22.45. REMOVED CORROSION IAW SRM 53-10-1 0.005. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 3 SHT 5. ALODINED SEAT TRACK IAW SRM 51-10-2, PRIMED IAW SRM 51-40-5.Mar 2, 2001 · N747DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001747510Seat Track · corrodedD-CHECK, SEAT TRACK SECTION BETWEEN STA 1030-970 LBL 45.0 HAS AREAS OF SURFACE CORROSION 69-46, 47. REMOVED CORROSION IAW SRM 53-10-1 0.005 MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 3 SHT 5. ALODINED SEAT TRACK IAW SRM 51-10-2. PRIMED IAWMar 2, 2001 · N747DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001747523Seat Track · damagedD-CHECK, SEAT TRACK SECTION STA 680-500 RBL 45.5 HAS SURFACE CORROSION. SEAT TRACK GOUGED AND OUT OF LIMIT, STA 665.SEAT TRACK FLANGE CORRODED.Feb 22, 2001 · N747DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001747513Seat Track · corrodedD-CHECK, SEAT TRACK SECTION STA 1034 AND FWD 1050-1070 RBL 22.45 CORRODED. SEAT TRACK IS VISUALLY OUT OF ALLOWABLE DAMAGE LIMITS AT FS 1040, 1053, AND 1060 RBL 22.45 PER SRM 53-10-1 FIG 3.Feb 22, 2001 · N747DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001747520Floorbeam · corrodedD-CHECK, FLOORBEAM TOP CAP STA 1110 BL 0 CORRODED AROUND FASTENER HOLE.Feb 12, 2001 · N747DH · Boeing 727200 · Fuselage Main, Floor BeamSDR DHL2001747519Skin · damagedD-CHECK, LEFT WING INBD L/E OF WING-TIP EXISTING REPAIR DAMAGED. REMOVED EXISTING FILLER REPAIRED MINOR DENT AND GOUGE IAW 727 SRM 51-40-01 PG 1-5.Feb 12, 2001 · N747DH · Boeing 727200 · Wing, Plate/SkinSDR DHL2001747517Stringer · crackedD-CHECK, STRINGER 15L STA 720B CRACKED. CUT OUT DAMAGED AREA OF STRINGER PER SRM 53-10-3 FIG 5. HFEC PER BOEING NDT PART 6, 51-00-00. INSTALLED REPAIR PARTS PER SRM 53-10-3 FIG 5.Feb 12, 2001 · N747DH · Boeing 727200 · Fuselage Main, Longeron/StringerSDR DHL2001747516Stringer · crackedD-CHECK, STRINGER 16L STA 354.2-344 CRACKED. REMOVED DAMAGE ON INTERCOASTAL IAW SRM 51-40-2. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2.Feb 12, 2001 · N747DH · Boeing 727200 · Fuselage Main, Longeron/StringerSDR DHL2001747514Floor Support · corrodedD-CHECK, FLOORBOARD SUPPORT AT APPROX STA 1034 RBL 22.45 CORRODED AROUND FASTENER HOLE. REMOVED CORROSION PER 51-10-6.Feb 12, 2001 · N747DH · Boeing 727200 · Fuselage Miscellaneous StructureSDR DHL2001747511Seat Track · corrodedD-CHECK, SEAT TRACK SECTION 930-870 LBL 45.5 HAS AREA OF SURFACE CORROSION. REMOVED FASTENERS ON SEAT TRACK TO CLEAN UP CORROSION PER SRM 51-30-2. CLEANED CORROSION ON SEAT TRACK PER SRM 51-10-6, SEAT TRACK WITHIN LIMITS IAW SRM 53-10-1 PG 15-16. ALODINE TRFeb 12, 2001 · N747DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00396Accessory Unit · inoperativeON GEAR EXTENSION ON APPROACH TO OAK, GEAR GREEN LIGHTS ALL CAME ON WITH ALL E DOOR RED LIGHTS AND TAILSKID LIGHT ON. MADE LOW APPROACH AND GOT GPWS VOICE TO LOW GEAR WAVED OFF, FOLLOWED RED TABS. SLOWED TO 200 KNOTS, LOWERED GEAR AND ALL IND NORMAL. REMOVEJun 21, 2000 · N235 · Boeing 727200 · Landing Gear Position and WarningSDR 02FDEA00320Light · inoperativeDURING APPROACH TO CLE, L GEAR DOWN INDICATOR LIGHT (GREEN) DID NOT ILLUMINATE; NO OTHER ABNORMAL INDICATIONS. UNABLE TO REMOVE BULBS TO REPLACE. RECEIVED VISUAL CONFORMATION FROM TOWER THAT GEAR WAS DOWN; LANDED NORMALLY. RELAMPED ANNUNCIATOR. LIGHTS TESMay 8, 2000 · N135FE · Boeing 727200 · Landing Gear Position and WarningSDR 99ZZZX2962Seam · failedDURING FLIGHT ATTENDANT TRAINING, SLIDE INFLATED FOR APPROXIMATELY 10 MINUTES. SEAM AT UPPER AFT CORNER SPLIT, DEFLATING SLIDE.Jul 13, 1999 · Boeing 727200 · Escape SlideSDR 99ZZZX2963Life Raft · failedDURING FLIGHT ATTENDANT TRAINING, LIFE RAFT INFLATED ONLY HALF-WAY.Jul 12, 1999 · Boeing 727200 · Life RaftSDR 99ZZZX253Wheel · crackedCRACK DETECTED VISUALLY AND CONFIRMED BY EDDY CURRENT AT THE BOLT BOSS AREA. NO CRACK PERMITTED THIS AREA. B.F. GOODRICH OVERHAUL MANUAL 32-40-21 REV 3 DATE 4-30-83. INSPECTION SECTION PARA 2B.Dec 28, 1998 · Boeing 727200 · Wheel/Ski/FloatSDR UPS97224089Battery · dischargedINSPECTION TYPE-N/A, SEVERAL EMER EXIT LIGHTS DIM. REPLACED 11 EXIT LIGHT BATTERIES THROUGHOUT THE CABIN. CHECK OK IAW TPCR 2-33-MM-97-4082.Aug 10, 1997 · Boeing 727200 · Emergency LightingSDR CA970811003Engine · making metal(CAN) ON DESCENT #3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED, ACCOMPANIED WITH A DROP IN OIL PRESSURE INDICATION. THE FLIGHT CONTINUED WITH THE OIL PRESSURE LIGHT BEING EXTINGUISHED BY MANIPULATION OF THE #3 ENGINE THRUST LEVER. POST FLIGHT INSPECTION FOUND TAug 7, 1997 · Boeing 727200 · Engine (Turbine/Turboprop)
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