Boeing 727-30C

Service difficulty reports · 931

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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 aircraft_model_key = '72730C'
  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 UPS01235978Web · crackedINSPECTION TYPE:C NR 3 SLAT ANTI ICE WEB IS CRACKED AT CUTOUT FOR ANTI ICE DUCT. REPAIRED IAW UPS AUTORIZATION B727-57-20028 AND SMRO EO 2001-016-006.May 11, 2001 · N906UP · Boeing 72730C · Leading Edge DevicesSDR UPS01235908Web · crackedINSPECTION TYPE:C STRUCTURE ABOVE NR 2 ENGINE, WEB CRACKED AT BS 1388 APPROX RT SIDE. NEW WEB INSTALLED IAW SRM 51-30-02 & BOEING DRAWING 65-17555.May 11, 2001 · N906UP · Boeing 72730C · Vertical StabilizerSDR UPS01235946Door Frame · crackedINSPECTION TYPE:C, SUSPECT CRACK IN LWR AFT CORNER OF FWD CARGO DOOR FRAME. REPLACED LWR AFT CORNER OF FWD CARGO DOOR FRAME IAW DRAWING 65-18620.May 10, 2001 · N906UP · Boeing 72730C · Cargo/Baggage DoorsSDR UPS01235979Fitting · crackedINSPECTION TYPE:C NDI ON BS 950 RT FITTING CONFIRMED CRACK ON OUTBOARD FLANGE BETWEEN S9R AND 10R. RT 950 FRAME FITTING REPLACED IAW UPS EO B727-5310-3011.May 9, 2001 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS01235975Beam · corrodedINSPECTION TYPE:C MCD UPPER BEAM AND UPPER BEAM DOUBLER CORRODED. DOOR REMOVED AND UPPER BEAM AND UPPER BEAM DOUBLER REPLACED.May 9, 2001 · N906UP · Boeing 72730C · Cargo/Baggage DoorsSDR UPS01235968Strap · crackedINSPECTION TYPE:C CRACK INDICATIONS IN REINFORCING STRAP AT MID GALLEY DOOR FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-2685.May 9, 2001 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS01235967Door Frame · crackedINSPECTION TYPE:C, CRACK ON AFT UPPER SECTION OF GALLEY DOOR FRAME. REPAIR CARRIED OUT IAW UPS EO B727-5240-4626.May 9, 2001 · N906UP · Boeing 72730C · Service DoorsSDR UPS01235953Stringer · corrodedINSPECTION TYPE:C, AREA OF SUSPECT CORROSION AT S4L BS 1185. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-00, 51-30-4.May 8, 2001 · N906UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS01235907Skin · damagedINSPECTION TYPE:C, FUSELAGE SKIN FOUND TO HAVE WEAR HOLE AT BS 1187 BETWEEN S24 LT & S26 LT SECT 48. REPAIR CARRIED OUT IAW SRM 53-30-3, 51-30-1, 51-20-00, 51-10-2.May 8, 2001 · N906UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL2001701009Actuator · failedRT MLG DID NOT GO DOWN. RT MLG EXTENDED WITH GOOD INDICATIONS AFTER COMPLETION OF ABNORMAL MANUAL GEAR EXTENSION. REPLACED RT MLG LOCK ACTUATOR PER B727 M/M 32-32-61. PERFORMED GEAR SWING AND OPS CK NORMAL PER 32-32-0 AND 32-61-00.May 8, 2001 · N701DH · Boeing 72730C · Landing Gear ActuatorSDR UPS01235877Bracket · crackedINSPECTION TYPE:C, WING TO BODY FAIRING ATTACH BRACKET BS 945 S18A LT CRACKED. NEW BRACKET FABRICATEDMay 7, 2001 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL2001701006Computer · defectiveAT FL330 AT M-805 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECT ON SERVO A. DEFERRED A MODE ON A/P PER DHL MEL 22-1-11A. PLACARD INSTALLED. REPLACED ROLL CHANNEL COMPUTER PER MM 22-11-111. OPS CHECKED GOOD.Apr 28, 2001 · N701DH · Boeing 72730C · Autopilot ComputerSDR DHL2001701005Bushing · out of adjA/C REQUIRES 5 DEG RT BANK TO MAINTAIN STRAIGHT FLIGHT. ADJUSTED ECCENTRIC BUSHINGS OF RIGHT WING INBOARD AFT FLAP PER MM 27-51-2.Apr 28, 2001 · N701DH · Boeing 72730C · Trailing Edge Flap Control SystemSDR DHL2001701007Sensor · looseAT FL330 AT M.78 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECTED ON SERVO-A. TIGHTENED CRANK ON A-SYS ELEVATOR POSITION SENSOR IAW B727 22-11-77 OP CK GOOD. NORMAL ON GROUND IAW B727 M/M 22-11-71.Apr 27, 2001 · N701DH · Boeing 72730C · Autopilot SystemSDR DHL2001702010Switch · stuckTAKEOFF WARNING HORN SOUNDED WHEN TAKEOFF THRUST WAS APPLIED WITH FLAPS AT 15, SPEED BRAKE STOWED, AND STAB TRIM AT 5.5. TAKEOFF WAS DISCONTINUED. FOUND TAKEOFF WARNING SWITCH STUCK. REMOVED AND REPLACED SWITCH. TESTED SYSTEM IAW DHL MM 27-51-191.Apr 24, 2001 · N702DH · Boeing 72730C · Trailing Edge Flap Control SystemSDR DHL2001702009Switch · out of adjTAKEOFF WARNING HORN SOUNDED DURING T/O ROLL 60 KTS. TAKEOFF REJECTED. VERIFIED T/O CONFIGURATION WAS CORRECTED. 2ND T/O NORMAL. FOUND SPEED BRAKE TAKEOFF WARNING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH S194 AND TESTED IAW MM 31-26-25 P401-403. OPS CHApr 11, 2001 · N702DH · Boeing 72730C · Drag Control SystemSDR DHL2001702007Windshield · failedL-2 WINDSHIELD CRACKED DURING CRUISE FLIGHT. CORRECTIVE ACTION: REPLACED L-2 WINDOW IAW B727 MM 56-12-11. OPS CK SERVICABLE PRESSURIZED A/C ON GROUND. NO LEAKS NOTED. STATUS CLOSED.Mar 30, 2001 · N702DH · Boeing 72730C · Passenger/Crew DoorsSDR UPS01235624Stringer · corrodedINSPECTION TYPE: C, FWD CARGO COMPT BETWEEN STA 680 AND 660, LT SIDE STRINGER 24, CORROSION. CUT OUT SECTION AT BAD STRINGER AREA STA 680 TO STA 660 LT STRINGER 24 INSTALLED REPAIR AS PER B727 SRM 53-10-3 FIG 1 SIDE OF STRINGER DOUBLER REPAIR 11 1/4 INCHESMar 29, 2001 · N918UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR DHL2001702008Gearbox · leakingIN CRUISE FLIGHT LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-40 PSI. PERFORMED OIL PRESS BELOW 40 PSI ABNORMAL CHECKLIST AND DISCOVERED ZERO OIL QUANTITY. PERFORMED IN FLIGHT ENG SHUTDOWN ABNORMAL PROCEDURE. OIL PRESS INDICATION ZEMar 29, 2001 · N702DH · Boeing 72730C · Accessory GearboxesSDR DHL2001701004Indicator · malfunctionedNR 3 LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAXI. QUANITY AND PRESS NORMAL. TRANSFERRED TO DMI PER MEL 79-4. VISUALLY VERIFIED OIL QUANITY FULL, CONTROL 4933 PLACARD INSTALLED BULB REMOVED. STATUS-OPEN.Mar 29, 2001 · N701DH · Boeing 72730C · Engine Oil PressureSDR UPS01235625Keelbeam · crackedINSPECTION TYPE:C, RT SIDE OF KEELBEAM APU CUT OUT FWD END HAS A DOUBLER CRACKED AT BS 874 NEXT TO HORIZONTAL STIFFENER. REMOVED OLD DOUBLER REPAIR OF KEEL BEAM AREA AND INSTALLED NEW DOUBLER REPAIR AT SAME AREA BS 874 AS PER B727 SRM 51-10-01.Mar 28, 2001 · N918UP · Boeing 72730C · Fuselage Main, KeelSDR UPS01235623Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX 770 AND LBL 13 WEB IS CORRODED. REMOVED WEB AT LOWER FUSELAGE CENTER SECTION AT BS 770 AND LBL13 WEB AS PER B727 SRM 51-30-02. REPLACED DAMAGE WEB LOWER CENTER WING AT BS 770 AND LBL 13 WEB AS PER B 7Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center BoxSDR UPS01235622Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX BETWEEN BS 800 TO 810 AND LBL 13 WEB IS CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN BS 800 TO BS 810 LBL 13 WEB AS PER B727 SRM 51-30-2. REPLACED DAMAGED WEB LOWER CENTER WING AT BSMar 27, 2001 · N918UP · Boeing 72730C · Wing, Center BoxSDR UPS01235621Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION BETWEEN BS 775 TO BS 800 AND RBL 13 WEBS CRACKED AND CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN 767 TO 830 RBL13 AS PER B727 SRM 51-30-02 REMEOVED AND REPLACED DAMAGE WEB LOWER CENTER WING Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center BoxSDR UPS01235628Seat Track · gougedINSPECTION TYPE: C, MAIN CARGO DECK FUSELAGE STATION 1130 LBL 45 SEAT TRACK TONGUES ARE NICKED AND GOUGED REPLACED DAMAGED SECTION OF SEAT TRACK FROM BS 1110 TO STA 1130 LBL 45Mar 26, 2001 · N918UP · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS01235626Pressure Panel · crackedINSPECTION TYPE: C, NOSE WHEEL WELL RT SIDE CRACKED AT BS 286.5 TO BS 294.5 WL 160 LOOKING FROM INSIDE TUNNEL. CUT OUT DAMAGE AREA, NDT CUT OUT, AND INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 FIG.1Mar 26, 2001 · N918UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL2001702006Bolt · shearedMAIN CARGO DOOR WILL NOT CLOSE.CORRECTIVE ACTION: REPLACED SHEARED BOLTS AT FWD CAM LATCH PER MM 52-34-21. OPS CHECK GOOD. STATUS CLOSED.Mar 23, 2001 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR DHL2001703002Indicator · inoperativeA-SYSTEM HYDRAULIC QUANTITY INDICATOR INOP. PLACED ON DEFERRAL PER DMI 4858. MEL REF 29-14 CAT C.Mar 23, 2001 · N703DH · Boeing 72730C · Hydraulic Indicating SystemSDR UPS01235327Oxygen Mask · failedD-SECOND OBSEVERS. O2 MASK INOP M-211583. R & R 02 MASK & CLEANED AUDIO JACK. CHECKS GOOD THIS CLEARS DFRL.Mar 21, 2001 · N917UP · Boeing 72730C · Crew Oxygen SystemSDR UPS01235279Frame · crackedINSPECTION TYPE:C-CK, CRACK AT FUSELAGE FRAME BS 930 ABOVE STR 13L. CUT OUT DAMAGE SECTION OF FRAME BETWEEN STR 12L & 13L. INSTALLED FORMED ANGLE REPAIR, HEAT TREATED.Mar 5, 2001 · N919UP · Boeing 72730C · Fuselage Main, FrameSDR DHL2001702003Pump · failedNR 2 ENGINE FAILURE ON TAKEOFF ROLL AT 90 KTS. REMOVED AND REPLACED FUEL PUMP. FUEL CONTROL UNIT CHECKS GOOD PER M/M 73-11-1 & 72-00.Mar 2, 2001 · N702DH · Boeing 72730C · Engine Fuel PumpSDR UPS01235278Stringer · corrodedINSPECTION TYPE:C-CK, STRINGER 18 LEFT CORRODED BETWEEN BS 440 TO BS 460. REMOVED CORROSION ON STRINGER FLANGE. FOUND OUT OF UNIT. INSTALLED STRINGER REPAIR.Feb 28, 2001 · N919UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS01235113Light · inoperativeINSPECTION TYPE:PFLT, ON PREDEPT CK FOUND COCKPIT EMERGENCY EXIT ASSY INOP IN ARM OR ON. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CHECK OK.Feb 28, 2001 · N906UP · Boeing 72730C · Emergency LightingSDR DHL2001701003Indicator · defectiveNR 2 OIL PRESURE GAUGE BEGAN READING 20 PSI AT POSITION AND HOLD. PULLED-OFF RUNWAY AND SHUTDOWN ENGINE NR 2. TROUBLESHOT SYSTEM AND FOUND NR 2 ENGINE OIL PRESSURE INDICATOR DEFECTIVE. REMOVED AND REPLACED NR 2 OIL PRESSURE INDICATOR. RAN ENGINE, SYSTEM OPFeb 28, 2001 · N701DH · Boeing 72730C · Engine Oil PressureSDR UPS01235402Fitting · crackedINSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CRACK MIGRATING FROM OB BOLT. REMOVED FITTING LT WING FRONT SPAR INTERIOR LBL 70.5 V SHAPE. INSTALLED LT WING UPPER FRONT SPAR CONER NEW FITFeb 26, 2001 · N919UP · Boeing 72730C · Wing, Attach FittingsSDR DHL2001701002Support Fitting · crackedDURING A POST-MOD INSPECTION OF PYLON, CRACKS WERE FOUND IN FWD ENGINE SUPPORT FITTING UPPER FLANGE BOLT HOLES E AND F. REPAIRED NR 3 ENGINE PYLON AT BOLT HOLES E AND F, IAW BOEING MESSAGE CPZ-OSC-01-00017H APPROVED AS ALTERNATE MEANS OF COMPLIANCE TO AD 97-0Feb 23, 2001 · N701DH · Boeing 72730C · Nacelle/Pylon, Attach FittingsSDR DHL2001703001Skin · corrodedSTRINGER 19 RIGHT AT FS 369 TO FS 400 LAP SEAM HAS BULGING SKIN AROUND SEVERAL FASTENERS. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER 12.55 X 7.05 INCH DOUBLER. REWORKED LAP AT STA 360 TO 390 WORK DONE IAW SRM 53-30-3.Feb 20, 2001 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS01235399Duct · crackedINSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS. 1 EA 4 INCH CRACK 93 INCHES FROM AFT EDGE 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR.Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake SystemSDR UPS01235398Duct · crackedINSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS 2 EA APPX 100-104 INCH FROM AFT EDGE. 1 EA 7 INCH Y SHAPED CRACK & 1 EA 1.5 INCH CRACK APPX 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR. HEAT TREATED.Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake SystemSDR UPS01235284Intake Duct · crackedINSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 6 INCH CIRCUMFERENTIAL CRACK AT 4 O''CLK APPROX 30 INCHES AFT OF WHERE S-DUCT ATTACHES TO INLET. CUT OUT DAMAGED AREA APPROX 7 X 1 INCHES. PERFORMED NDT AND NO CRACK INDICATIONS. INSTALLED SKFeb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake SystemSDR UPS01235283Skin · crackedINSPECTION TYPE:C-CK, FUSELAGE SKIN HAS CORROSION BULGE AND APPROX 3 INCH LATERAL CRACK. REMOVED FASTENERS, REMOVED CORROSION. NDT INSP C/W CUT DAMAGE AREA AND INSTALL DOUBLER REPAIR AT FUSE SKIN.Feb 19, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS01235282Skin · corrodedINSPECTION TYPE:C-CK, LOW FREQ EDDY CURRENT INSP OF SKIN AT BS 441 BETWEEN STRG 18R & 19R HAS INDICATION OF CORROSION LOSS GREATER THAN 10 PERCENT. REMOVED EQUIPMENT TO ACCESS REPAIR, CUT DAMAGED AREA AND INSTALLED REPAIR PER EO -1371.Feb 19, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR UPS01235221Duct · crackedINSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AFT EDGE AT 3 O''CLOCK. CUT OUT DAMAGE AREA. INSTALLED REPAIR.Feb 19, 2001 · N919UP · Boeing 72730C · Nacelle/Pylon, Main FrameSDR UPS01235401Lap Joint · bulgedINSPECTION TYPE:C CK LAP JOINT 19RT HAS SKIN BULGE AT BS 620. CUT OUT DAMAGED SKIN LWR & UPPER AREA. INSTALLED REPAIR PART AT LAP JOINT STR 19 BS 620.Feb 18, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL2001702004Floorbeam · corrodedAT FS 1050 LBL 3 ON BOTTOM OF FLOORBEAM WL 200 CORROSION ON FLOORBEAM AND GILLINER ATTACH ANGLE. REMOVED AND REPLACED LOWER SUPPORT TEE.Feb 17, 2001 · N702DH · Boeing 72730C · Fuselage Main, Floor BeamSDR DHL2001702005Seat Track · damagedSIDE BASH BAR NR 3 AND 4 MUSHROOM OUT OF FLOOR TRACK. REMOVED AND REPLACED FLOOR TRACK FROM STA 480 TO 560 PER SRM 53-10-2 AND 53-10-5.Feb 17, 2001 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR UPS01235400Frame · crackedINSPECTION TYPE:C CHECK LT W/W LWR SECTION OF BS 930 FRAME SHOWS CRACK TO AFT CENTER SECTION WHERE REPAIR NOT INSTALLED. ACCOMPLISHED STA 930 RT & LT FRAME REMOVAL & REPLACEMENT.Feb 15, 2001 · N919UP · Boeing 72730C · Fuselage Main, FrameSDR UPS01234996Light · inoperativeINSPECTION TYPE:IN ON PREFLIGHT CHECK EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WOULD NOT TEST WITH EMERGENCY EXIT LIGHT SWITCH ON O/H. LIGHTS WORK OK AT LIGHT ASSY W/SWITCH ON. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT COCKPIT DOOR. OPS CHECK OK PER MFeb 15, 2001 · N906UP · Boeing 72730C · Emergency LightingSDR DHL2001701001Skin · delaminatedREFERENCE DMI 4025 RT O/B MID FLAP INSP OF REPAIR NEXT 30 DAYS AT 5 DAY INTERVALS TILL REPAIR COMPLETED. REMOVED TEMP REPAIR, INSTALLED PERM REPAIR RT O/B MID FLAP THAT WAS DELAMINATED, IAW BOEING 727 SRM 51-40-20.Feb 12, 2001 · N701DH · Boeing 72730C · Trailing Edge FlapsSDR DHL2001702002Warning System · false activationDISCONTINUED TAKEOFF DUE TO TAKEOFF WARNING HORN. FLAPS, SPEEDBRAKE AND TRIM ALL PROPERLY SET. PERFORMED T/O WARN TEST PER MM 31-26-0 PARA 6, TEST OK.Jan 30, 2001 · N702DH · Boeing 72730C · Central Warning
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