Boeing 727-155C

Service difficulty reports · 153

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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 = '727155C'
  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 DHL2002715010Warning System · malfunctionedRTO AT CVG MAXIMUM ATTAINED AIRSPEED 5 KIAS. UPON INITIATION OF TO THRUST, THE TO WARNING HORN SOUNDED. AFTER TAXIING CLEAR OF THE RUNWAY, NOTIFIED FLIGHT CONTROL AND ADVISED THEM OF THE PROBLEM. MX CONTROL HAD BEEN NOTIFIED PRIOR TO CALLING FC. AFTER WE MOOct 22, 2002 · N715DH · Boeing 727155C · Central WarningSDR DHL2002715009Switch · dirtyT/O WARNING HORN SOUNDED ON T/O ROLL. CLEANED CONTACTS ON AIRBRAKE POSITION SWITCH IN FWD NOSE BAY. OPS CHECK GOOD IAW 31-26-00.Jun 19, 2002 · N715DH · Boeing 727155C · Central WarningSDR DHL2002715008Warning System · malfunctionedWHILE BRINGING POWER UP FOR TAKEOFF WITH AIRCRAFT CONFIGURED, GOT CONFIGURATION HORN AND SYSTEM THEN TESTED BAD ON TAXIWAY. ABORTED TAKEOFF. CYCLED FLAPS, TAKEOFF WARNING SYSTEM, OPS CHECKS GOOD IAW MM 31-26-00.May 29, 2002 · N715DH · Boeing 727155C · Central WarningSDR DHL2002715007Power Unit · failedAPU FIRE WARNING BELL IN COCKPIT INOP, HORN IN NOSE WHEEL WELL WORKS NORMALLY. REMOVED APU FIRE DETECTION POWER UNIT AND CLEANED CONTACTS. REINSTALLED POWER UNIT. OPS CHECK GOOD IAW MM 26-15-00.May 3, 2002 · N715DH · Boeing 727155C · Fire DetectionSDR DHL2002715006Warning System · activatedTAKEOFF REJECTED FOR AURAL WARNING HORN. CYCLED FLAPS AND SPEED BRAKE, VERIFIED MOVEMENT OF FLT CONTROL SURFACES. PERFORMED AURAL OPERATIONAL CHECKOUT IAW 31-26-0. OP CHECK GOOD.Apr 23, 2002 · N715DH · Boeing 727155C · Central WarningSDR DHL2002715005Warning Horn · failedDURING APU FIRE WARNING TEST, FIRE BELL AND FIRE WARNING HORN FAIL SOUND. REMOVED AND REPLACED FIRE WARNING HORN IN NOSE WHEEL WELL IAW MM 26-11-00. OPS CHECK GOOD.Apr 13, 2002 · N715DH · Boeing 727155C · Fire DetectionSDR DHL2002715004Fitting · crackedREPLACE MAIN CARGO DOOR LATCH FITTING. GAINED ACCESS TO MCD LATCH SUPPORT FITTING AT B.S. 580 THROUGH FWD. CARGO PIT LT SIDEWALL/ CEILING AND MAIN CABIN. REMOVED AND REPLACED MCD LATCH SUPPORT FITTING AT BS 580. ADJUSTED LATCH FITTING AND OPS CHECKED. OPENApr 10, 2002 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL2002715003Angle · crackedOn weekly visit "discrepancy" Frame at door latch fitting is cracked in radius at BS 500, 4l 200, below S-17L.1) Upon further evaluation found attach angle "T" to frame cracked. Removed frame to skin attach "T" I.A.W. 727 S.R.M. 51-30-2. Fabricated attach anglApr 8, 2002 · N715DH · Boeing 727155C · Fuselage Main, StructureSDR DHL2002715002Power Supply · inoperativeAPU FIRE DETECTION SYSTEM WILL NOT TEST. TROUBLESHOT SYSTEM, REMOVED AND REPLACED APU FIRE DETECT OPERATING POWER SUPPLY. OPERATIONAL CHECK OF SYSTEM GOOD MM REF 26-15-00.Feb 2, 2002 · N715DH · Boeing 727155C · Fire DetectionSDR DHL2002715001Power Unit · inoperativeAPU FIRE TEST WILL NOT TEST. REPLACED APU FIRE DETECTION POWER UNIT IAW B727 M/M 26-15-00, OP CHECK GOOD.Jan 29, 2002 · N715DH · Boeing 727155C · Fire DetectionSDR DHL2001715011Computer · faultyWITH AUTO PILOT ENGAGED RAPID DEFLECTION OF CONTROL WHEEL OCCURS BOTH LEFT AND RIGHT OF ABOUT 10 DEGREES. DEFERRED AUTO PILOT SYSTEM AND MX CONTROL WAS NOTIFIED. REMOVED AND REPLACED ROLL CHANNEL COMPUTER, OPS CHECKS GOOD IAW B727 MM 22-11-111.Dec 1, 2001 · N715DH · Boeing 727155C · Autopilot ComputerSDR DHL2001715010Skin · damagedBELOW RIGHT CORNER OF MAIN CARGO DOOR (APPROX 3 FEET) A 4 INCH BY 1/4 GASH IN SKIN APPROX 1/4 DEEP. AREA IS ALSO DENTED, ALSO 2 AREAS ADJACENT TO GASH ARE DOWN TO BARE METAL. CUTOUT DAMAGED AREA. FABRICATED DOUBLER REPAIR & FILLER. REPAIR MADE TO DAMAGED SKIN Aug 10, 2001 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL2001715009Warning System · malfunctionedTAKEOFF WARNING CAME ON AT THE TAKEOFF ROLL, TAXIED CLEAR OF THE RUNWAY AND CYCLED THE FLAPS,TRIM AND SPEED BRAKE SYSTEM WENT BACK TO NORMAL. PERFORMED TAKEOFF WARNING SYS TEST CHECKS GOOD IAW B-727 M/M 31-26-0.Aug 8, 2001 · N715DH · Boeing 727155C · Central WarningSDR DHL2001715008Downlock SwitchDURING GEAR EXTENSION @ CVG LT. MAIN GEAR LIGHT DID NOT ILLUMINATE. RED LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, PROBLEM WAS NOT CORRECTED.R&R'D LEFT MAIN GEAR DOWNLOCK SWITCH IAW B-727 M/M 32-09-211. OP CHECKS SERVICEABLE.Jun 30, 2001 · N715DH · Boeing 727155C · Landing Gear Position and WarningSDR DHL2001715007Computer · faultyWITH AUTOPILOT A SERVO SELECTED, A/C PITCHES UP AND DOWN. OK WITH SERVO B SELECTED. DEFFERED AUTO PILOT A-MODE PER MEL 22-1-11A, CAT C, DMI 6211. PLACARDS INSTALLED. T/S SYS ORDERED PITCH COMPUTER. PARTS IN CVG AS PER MXC DMI 6211 CONTINUES. REMOVED ANDJun 29, 2001 · N715DH · Boeing 727155C · Autopilot ComputerSDR DHL2001715006Computer · malfunctionedON CLIMBOUT IN A-MODE AUTOPILOT PORPOISED. REPLACED PITCH CHANNEL PER MM 22-11-101. OPS CKS GOOD. THIS CLEARS DMI 5771.May 26, 2001 · N715DH · Boeing 727155C · Autopilot ComputerSDR DHL2001715005Receiver · unserviceableAUTOPILOT WILL NOT TRACK VOR IN NAV/LOC MODE. REPLACED NR 1 NAV RCVR PER MM 34-31-21, OPS CKS GOOD. THIS CLEARS DMI 5772.May 26, 2001 · N715DH · Boeing 727155C · Localizer/VOR SystemSDR DHL2001715004Sill · crackedFAA INSPECTION FOUND LWR BELLY DOOR FWD THRESHOLD SILL-PLATE CRACKED.REMOVED OLD SILL-PLATE AND INSTALLED SERVICABLE PLATE IAW M/M 53-13-0. STATUS-CLOSED.Apr 10, 2001 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL2001715003Bearing · separatedVIBRATION DURING TAXI AND A/C REQUIRES HIGHER THAN NORMAL THRUST TO TAXI. NR 1 MAIN TIRE NUT AND BEARING SEPERATED. REPLACED LT MLG LOWER CYLINDER ASSY. FOUND NR 1 MAIN T/W ASSY SLEEVE DAMAGED. REPLACED NR 1 T/W ASSY, NR 1 BRAKE, AND NR 2 W/T ASSY.Mar 27, 2001 · N715DH · Boeing 727155C · Wheel/Ski/FloatSDR DHL2001715001Bulb · burned outUPPER MAIN CARGO SMOKE DETECTORS NOT VISIBLE. RELAMPED UPPER SMOKE DETECTOR. OPS CHECK GOOD I.A.W 26-17-01Jan 3, 2001 · N715DH · Boeing 727155C · Smoke DetectionSDR DHL2000715026Hinge · bentLOUD WHISTLE HEARD DURING CLIMBOUT, STARTED AT 2 PSI THEN GEAR WARNING HORN SOUNDED. WHISTLE STOPPED AT 6 PSI DURING DECENT. FOUND L-1 ENTRY DOOR SEAL PULLED OUT 3 TO 4 INCHES ON LOWER AFT END. THE LOWER HINGE FLAPPER IS BENT. R&R LOWER HINGE FLAPPER.Dec 13, 2000 · N715DH · Boeing 727155C · Passenger/Crew DoorsSDR DHL2000715003Doubler · damagedPANEL NUMBER 9216 HAS INTERNAL REPAIR CRACKED. REPLACED DOUBLER. SIZE OF REPAIR 6 X 4.5 INCHES.Oct 27, 2000 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL2000715006Angle · corrodedFAIRING SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE BS 660 UNDER STRINGER 27R. INSTALL REPAIR PER B727 SRM 51-40-3, 51-10-2. MATERIAL SIZE 30 X 2 INCHES.Oct 23, 2000 · N715DH · Boeing 727155C · Aerodynamic FairingsSDR DHL2000715025Panel · corrodedCORROSION AT FAIRING PANEL 3430 FWD FLANGE LOCATED AT BS 660. INSTALL REPAIR PER B727 SRM 53-10-01, 51-40-3. SIZE OF MATERIAL USED 30 X 2 INCHES.Oct 21, 2000 · N715DH · Boeing 727155C · Aerodynamic FairingsSDR DHL2000715024Angle · bentMCD TOP CUTOUT HAS A ANGLE WITH DENT AND BENT AT BS 600. REPLACED ANGLE PER B727 SRM 51-10-1 & 2. SIZE OF MATERIAL 12.5 X 6 INCHES.Oct 12, 2000 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL2000715023Structure · damagedMCD HAS ALUMINUM SHEET WITH EXCESS HOLES BS 620 (VERTICAL). REPAIRED PER B727 SRM 51-10-1 & 2, 51-30-2. SIZE OF MATERIAL USED 21 X 3.5 INCHES.Oct 12, 2000 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL2000715022Angle · crackedM.C.D. HAS ALUMINUM SEAL PROTECTOR CHAFED AND CRACKED AT LOWER END. REMOVED AND REPLACED SEAL PROTECTOR PER B727 SRM 51-30-2, 51-40-3.Oct 12, 2000 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL2000715012Structure · chafedMAIN CARGO DOOR FWD CUTOUT HAS VERTICAL STRIP CHAFED BS 480 S-6L. FABRICATED AND INSTALLED NEW FRAME PER B727 SRM 51-40-3. SIZE OF REPAIR 8 X 28 INCHES.Oct 12, 2000 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL2000715010Door Frame · bentMAIN CARGO DOOR UPPER AFT FRAME FOUND BENT. FABRICATED AND INSTALLED NEW UPPER AFT FRAME PER B727 SRM 51-30-2 AND 51-10-3. SIZE OF REPAIR 8 X 28 INCHES.Oct 12, 2000 · N715DH · Boeing 727155C · Fuselage Main, StructureSDR DHL2000715021Floor Support · crackedLOWER AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 1090 AND BBL 27. INSTALL NEW ANGLE SUPPORT PER B727 SRM 51-30-2, 53-10-1 AND -2. SIZE OF MATERIAL USED 1.75 X 6 INCHES.Oct 11, 2000 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL2000715020Floor Support · crackedLOWER AFT CARGO COMP FLOOR SUPPORT ANGLE CRACKED AT BS 1070 AND RBL 27. INSTALLED NEW SUPPORT ANGLES PER B727 SRM 51-30-2, 51-10-1 AND -2. SIZE OF MATERIAL USED 5 X 6 INCHES AND 5 X 3 INCHES.Oct 11, 2000 · N715DH · Boeing 727155C · Fuselage Miscellaneous StructureSDR DHL2000715005Fitting · crackedMAIN CARGO DOOR LATCH FITTING STA 580 UPPER FLANGE CRACK. INSTALLED ANGLE REPAIR PER BOEING TELEX DHL-MIA-00-00033H. SIZE OF REPAIR 7 X 2 X 3 INCHES.Oct 11, 2000 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL2000715019Skin · corrodedNR 2 CARGO DOOR HAS EXTERNAL SKIN WITH CUTOUT AT AFT EDGE BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER B727 SRM 52-00-2 AND 52-00-3. SIZE OF DOUBLER 15 X 4 INCHES.Oct 10, 2000 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL2000715011Panel · damagedNR 3 ENGINE PYLON FIXED COWL PANEL DAMAGED UPPER SIDE AFT OF 2ND VERTICAL LATCH CUTOUT. REPAIR PER SRM 51-10-1. SIZE OF REPAIR 23 X 4 INCHES.Oct 10, 2000 · N715DH · Boeing 727155C · Nacelle/Pylon, Plate/SkinSDR DHL2000715018Bulkhead · crackedFWD PRESSURE BULKHEAD BS 178 IS CRACK AT RBL 02 AND WL 196. INSTALLED DOUBLER REPAIR PER SB-727-53-0213. SIZE OF MATERIAL 9.6 X 132 INCHES.Oct 9, 2000 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL2000715017Bulkhead · crackedFWD PRESSURE BULKHEAD BS 178 IS CRACK AT RBL 10 AND WL 300. INSTALLED DOUBLER REPAIR PER SB-727-53-146. SIZE OF DOUBLER 6 X 7 INCHES.Oct 9, 2000 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL2000715014Fitting · crackedLEFT WING I/B MID FLAP ROLLER SUPPORT FITTING HAS CRACK. FABRICATE AND INSTALL DOUBLER REPAIR PER B727 SRM 51-30-2, 57-50-4. SIZE OF MATERIAL USED 6 X 3 INCHES.Oct 9, 2000 · N715DH · Boeing 727155C · Trailing Edge FlapsSDR DHL2000715013Torque Tube · crackedFWD ENTRANCE FRONT CUTOUT ACCESS FOR VERTICAL TORQUE TUBE HAS TWO CRACKS. REMOVED AND REPLACED DAMAGED SECTION PER B727 SRM 51-30-2. SIZE OF MATERIAL USED 10 X 8 INCHES.Oct 9, 2000 · N715DH · Boeing 727155C · Passenger/Crew DoorsSDR DHL2000715007Bulkhead · crackedFWD PRESSURE BULKHEAD BS 178 IS CRACKED RBL 02 WL 196. CRACK IS 1.5 INCH LONG. INSTALLED DOUBLER PER B727 SRM 53-10-9 AND SB 727-53-043. SIZE OF REPAIR 7 X 9 INCHES.Oct 9, 2000 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL2000715002Web · crackedFWD ENTRY DOOR HAS TOP HORIZONTAL WEB CRACKED AFT TOP CORNER, SEE THROUGH INSPECTION HOLE. INSTALLED REPAIR AT UPPER AFT CORNER AS PER B727 SB 52-115 FIG 4 AND 5 AND SRM 51-30-2, 51-20-4 AND MM 21-30-0. SIZE OF REPAIR 13 X 4 INCH.Oct 9, 2000 · N715DH · Boeing 727155C · Passenger/Crew DoorsSDR DHL2000715004Skin · corrodedNOSE SECTION LT SIDE EXTERIOR BS 243.7 AND STR 26L SKIN BULGING, RIVETS PULLING THROUGH. INSTALLED DOUBLER REPAIR PER SRM 51-10-1 AND 51-30-2 AND 53-30-3 AND MM 52-82-0 AND 32-33-0. SIZE OF REPAIR 15 X 17 INCHES.Oct 8, 2000 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL2000715009Pressure Panel · crackedNOSE WHEEL WELL RIGHT SIDE PANEL LOWER BS 240.7 WL 150 CRACKED. INSTALL DOUBLER REPAIR PER B727 SRM 51-10-1. SIZE OF REPAIR 7.5 X 3.5 INCHES.Oct 6, 2000 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL2000715008Frame · crackedNOSE L/G WHEEL WELL LT SIDE PANEL TO LWR CHORD BS 248 WL 150 SHOWS CRACK RUNNING FROM RIVET IS ABOUT 1.5 INCH LONG. INSTALLED DOUBLER REPAIR PER B727 SRM 51-10-1. SIZE OF REPAIR 7 X 3.5 INCH.Oct 6, 2000 · N715DH · Boeing 727155C · Fuselage Main, FrameSDR DHL2000715016Pressure Panel · crackedNOSE WHEEL WELL RIGHT SIDE LATERAL WEB PANEL AT BS 285.5 SHOW CRACK RUNNING BETWEEN RIVETS. FABRICATED AND INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2, AND 51-10-2. SIZE OF MATERIAL USED 15 X 15.5 INCHES.Oct 5, 2000 · N715DH · Boeing 727155C · Fuselage Main, BulkheadSDR DHL2000715015Skin · damagedFUSELAGE SKIN CREASED AT ATA 1342 JUST ABOVE STR 20L. FABRICATED AND INSTALLED REPAIR PER B727 SRM 51-30-2, 51-10-1, 53-30-1 AND 53-30-3.Oct 5, 2000 · N715DH · Boeing 727155C · Fuselage Main, Plate/SkinSDR DHL2000715001Outflow Valve · failedWHILE OPERATING ON RT PACK, A/C CABIN ALTITUDE REACHED 9800 FT AND CONTINUED TO CLIMB UNTIL DECENDED TO 10,000 FT. AT 10,000 FT CABIN STABILIZED AT 1.0 PSI/8000 FT, IN BOTH AUTO AND MAN MODE. DEFERRED PER MEL 21-16-1C. RT OUTFLOW VALVE REMOVED AND A/C FLEW Sep 7, 2000 · N715DH · Boeing 727155C · Pressure Regulator/Outflow ValveSDR DHL99715001Hinge · damagedMAIN CARGO DOOR HINGE ACTUATORS ATTACH POINT HOLES ELONGATED. FABRICATED AND REPAIRED HOLES AND PARTS PER TIMCO EO W00001 REV C AND BOEING SRM 51-10-7.Oct 15, 1999 · N715DH · Boeing 727155C · Cargo/Baggage DoorsSDR DHL9871520CAngle · crackedAT C-CHECK, LEFT WING NR 2 SLAT ACTUATOR COVER DOOR BOTH ATTACH ANGLE I/B AND O/B ARE CRACKED AT FWD END. REMOVED AND REPLACED ATTACH ANGLES PER SRM 51-40-4, 11 INCHES LONG. N/R 1112Oct 29, 1998 · N715DH · Boeing 727155C · Leading Edge Slat ActuatorSDR DHL98715004Duct · brokenNR 7 SLAT DID NOT RETRACT WITH FLAPS SELECTED TO UP. ABNORMAL ROLL INDICATION. FOUND WING ANTI-ICING TELESCOPING DUCT ON NR 7 SLAT BROKEN AND HANGING OUT. REMOVED DUCT AND INSTALLED BLANKING PLATES PER MEL. CLOSED ANTI-ICING SHUTOFF VALVES IN STUB WINGS.Oct 29, 1998 · N715DH · Boeing 727155C · Airfoil Anti/De-ice SystemSDR DHL9871528CWeb · crackedAT C-CHECK, VERTICAL WEB CRACKED AT BOTTOM LIGHTENING HOLES AT BS 1263 RT SIDE OF AFT AIRSTAIRS AREA. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 2 X 6. N/R 3185Oct 19, 1998 · N715DH · Boeing 727155C · Fuselage Miscellaneous Structure
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