Boeing 727-228

Service difficulty reports · 1,323

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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 = '727228'
  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 DHL2002721010Seat1) CAPTS SEAT BACK WILL NOT STAY UPRIGHT WHEN SOME PRESSURE IS APPLIED2) INSTALLED CAPT SEAT IAW B-MM 25-10-42 OPS CHECK GOODNov 16, 2002 · N721DH · Boeing 727228 · Cabin Equipment/FurnishingsSDR DHL2002721009Screw1) CAPTAINS SEAT BACK ADJ. DOES NOT COMPLETLY RELEASE MAKING IT DIFF. TO MOVE IN EITHER DIRECTION2) DEFFERED RECLINE PORTION OF SEAT IAW MEL 25-20-3 DMI 10980 ASSIGNED PER MAINT CONTROL-SEAT REPLACEMENT SCHEDULED3) REFER TO DMI #10980 CAPT SEAT BACK ADJUSTMNov 15, 2002 · N721DH · Boeing 727228 · Cabin Equipment/FurnishingsSDR DHL2002727012Switch · dirty1) APU FIRE TEST INOPERATIVE. DEFERRED PER MEL 49-1 CAT C DMI 10938 PLACARD INSTALLED. DEFFERED BY 34518. CLEANED FIRE TEST SWITCH, INSPECTED BALANCE OF APU FIRE DETECTION SYSTEM, APU FIRE TEST OPERATES NORMAL IAW GMM 26-15-00, THIS CLEARS DMI 10938 PLNov 9, 2002 · N727DH · Boeing 727228 · Fire DetectionSDR DHL2002726006Smoke Detector1) FORWARD LOWER CARGO COMPARTMENT FIRE DETECTOR S/N 1698 INOP AMBER & GREEN LIGHTS ILLUMINATED ON DETECTION SYS DISPLAY.2) DEFERRED LOWER CARGO COMPARTMENT FIRE DETECTOR S/N 1698 PER DHL MEL 26-19-1 CAT B DMI#10927. PLACARD INSTALLED.3) REF. DMI #10927 "FONov 9, 2002 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2002727011Smoke Detector1) #2 L/H MAIN CABIN SMOKE DETECTOR IS INOP. 2) REMOVED AND REPLACED #1, L/H MAIN CARGO SMOKE DETECTOR IAW. B-727 M/M 26-17-0.Nov 4, 2002 · N727DH · Boeing 727228 · Smoke DetectionSDR DHL2002720521Stringer · corrodedDURING C CHECK, E/E COMPARTMENT STR 25 IS CORRODED THRU AT UPPER FLANGE BETWEEN FRAME STA. 460 AND 480. REPAIRED IAW SRM.Oct 22, 2002 · N720DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002720516Seat Track · damagedDURING C CHECK, MAIN CABIN SEAT TRACK DAMAGED LBL 62.5 BS 620. REPAIRED IAW SRM.Oct 22, 2002 · N720DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002720515Seat Track · damagedDURING "C" CHECK, MAIN CABIN SEAT TRACK DAMAGED BS 480 TO 560 LBL 45.5. REPAIRED IAW SRM.Oct 17, 2002 · N720DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002726005Fire Warning · malfunctionedAFTER APU SHUT DOWN FIRE WARNING ILLUMINATED WITH NO BELL. BELL WOULD NOT TEST. DISCHARGED BOTTLE EMERGENCY PROCEDURE. DEFERRED PER MEL 49-1 CAT. "C" PLACARD 10665 INSTALLED. MAINTENANCE WAS NOTIFIED. REF. DMI #10665 - AFTER APU SHUTDOWN FIRE WARNING LIGHT IOct 16, 2002 · N726DH · Boeing 727228 · Fire DetectionSDR DHL2002720530Skin · corrodedDURING C CHECK, LT WING UPPER SURFACE STRAP BULGED ABOVE FRONT SPAR AFT. OF NR 3 SLAT. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228 · Wing, Plate/SkinSDR DHL2002720528Spar · corrodedDURING C CHECK, LT WING FWD. SPAR UPPER CHORD IS CORRODED AT WS 130 UPPER SURFACE AT BULGED SEALANT. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228 · Wing SparSDR DHL2002720527Skin · corrodedDURING C CHECK, BULGED SKIN/DISHED FASTENER HEADS ALONG STR 8 L, BS 1330. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720524Stiffener · crackedDURING C CHECK, FUSELAGE AFT. PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBBL 24.6 CRACKED FROM LIGHTNING HOLE IN 2 PLACES WL 260. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002720522Stiffener · crackedDURING C CHECK, FUSELAGE. AFT. PRESSURE BULKHEAD, BS 1183 VERTICAL BEAM LBBL 36.2 CRACK INDICATION. WL 249. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002720519Stiffener · crackedDURING C CHECK, FUSELAGE. AFT. PRESSURE BULKHEAD BS 1183 VERTICAL BEAM RBBL 24.6 CRACKED FROM LIGHTNING HOLE WL 260 APPROX. REPAIRED IAW SRM.Oct 14, 2002 · N720DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002720509Rib · crackedDURING C CHECK, RT WING INTERNAL RIB W.S. 629.0 LWR. CHORD BY ST-8 RIB CRACKED. REPAIRED IAW SRM.Oct 13, 2002 · N720DH · Boeing 727228 · Wing, Rib/BulkheadSDR DHL2002720508Rib · crackedDURING "C" CHECK, RT WING INTERIOR RIB W.S. 601 LWR. CHORD ST-6 CRACK. REPAIRED IAW SRM.Oct 13, 2002 · N720DH · Boeing 727228 · Wing, Rib/BulkheadSDR DHL2002720507Stringer · crackedDURING "C" CHECK, RT WING INTERIOR WS 656.5 LWR. CHORD. PREVIOUS REPAIR ST-6 CRACKED. PASSING STOP HOLE. ALSO CRACK AT ST-8 LOCATION. REPAIRED IAW SRM.Oct 13, 2002 · N720DH · Boeing 727228 · Wing, Longeron/StringerSDR DHL2002720506Rib · crackedDURING "C" CHECK, RT WING INTERIOR RIB WS 686.5 BS 8 LOWER CHORD PREVIOUS REPAIR CRACK BEYOND STOP HOLE. REPAIRED IAW SRM.Oct 13, 2002 · N720DH · Boeing 727228 · Wing, Rib/BulkheadSDR DHL2002720525Skin · corrodedDURING C CHECK, LOWER FUSELAGE SKIN AT BS 350 TO 360 LBL 13 TO RBL 13 BULGING AROUND FASTENER HEADS. REPAIRED IAW SRM.Oct 12, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720518Fastener · damagedDURING C CHECK, DISHED FASTENERS AT BS 360 BUTT SPLICE STR 19L. REPAIRED IAW SRM.Oct 12, 2002 · N720DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002720503Skin · corrodedDURING "C" CHECK, FUSELAGE SKIN STATION 420, BUTTSPLICE BULGING SKIN AROUND FASTENERS. REMOVED FASTENERS IAW B-727 SRM 51-30-2 AND REPAIRED AREA DAMAGED SKIN, IAW SRM.Oct 12, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720531Skin · corrodedDURING C CHECK, RT LWR NOSE HAS AREAS OF BULGING SKIN AND DISHED FASTENERS STA. 294 TO 360. REPAIRED IAW SRM.Oct 11, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720520Structure · corrodedDURING C CHECK, T/E FALSE SPAR UPPER BEAM IS CORRODED AFT. OF RT MLG AFT. TRUNNION. REPAIRED IAW SRM.Oct 11, 2002 · N720DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL2002720511Lap Joint · crackedDURING C CHECK, FUSELAGE LONGITUDINAL LAP JOINT STR 4 RIGHT , BS 1070 CRACK INDICATION AROUND FASTENERS. REPAIRED IAW SRM.Oct 10, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720523Fitting · crackedDURING C CHECK, UT INSPECTION CRACK INDICATION B.S. 870 RT FITTING JUST ABOVE STR. 10 RT. REPAIRED IAW SRM.Oct 9, 2002 · N720DH · Boeing 727228 · Fuselage Main, Attach FittingsSDR DHL2002720526Pressure Panel · crackedDURING C CHECK, RT MLG WW BULKHEAD BS 870 HAS A CRACK APU LOAD CONTROL VALVE. REPAIRED IAW SRM.Oct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002720514Frame · dentedDURING "C CHECK", AFT. CARGO FRAME BS 950E AT STR 25 LT HAS A DENT INTO THE RADIUS. REPAIRED IAW SRM.Oct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002720512Frame · chafedDURING "C" CHECK, CABIN AREA, FRAME AT STA. 760 IS CHAFED THRU ABOVE ABOVE STR 4 RT. REPAIRED IAW SRM.Oct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002720505Frame · dentedDURING "C" CHECK, AFT. CARGO FRAME BS 950 F AT STR 24 LT HAS DENTS INTO THE RADIUS. REPAIRED IAW SRM.Oct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002720504Stringer · corrodedDURING "C" CHECK, AFT. CARGO STR. 18 LT HAS CORROSION FROM BS 1166 TO BS 1183. REMOVED DAMAGE STRINGER IAW B-727 SRM 51-30-2 DIM. 12 INCH LONG. FABRICATED NEW STRINGER.Oct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002720502Frame · dentedDURING "C" CHECK, AFT. CARGO FRAME BS 970 AT STR. 24 LT HAS A DENT INTO THE RADIUS. REMOVED PREVIOUS REPAIR AND CUT-OUT DAMAGED AREA DIM 2 1/2 X 1 INCH IAW SRM FAB. REPAIR DIM 18 X 2 1/2 INCH IAW SRM. PART ALODINED AND PRIMED IAW. INSTALL DOUBLER AFT. COct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002720501Frame · dentedDURING "C" CHECK, DISCREPANCY AS FOLLOWS, IN FWD. CARGO FRAME AT BS 640 AT STR 24 R HAS A DENT INTO THE RADIUS. REMOVED PREVIOUS REPAIR IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AREA PIN 2 X 1 INCH AND FABBED DOUBLER. IAW B-727 SRM 53-10-4 FIG.1 3) PART ALOOct 7, 2002 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002720529Stiffener · crackedDURING C CHECK, VERTICAL STIFFENER IS CRACKED ON LEFT WING FRONT SPAR, LOWER END. LWS 130. REPAIRED IAW SRM.Oct 6, 2002 · N720DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL2002720517Skin · delaminatedDURING C CHECK, RT WING OUT FLAP. AFT SECTION SHOWS DELAMINATION AREA TOP SIDE WBL 440 APPROX. REPAIRED IAW SRM.Oct 5, 2002 · N720DH · Boeing 727228 · Trailing Edge FlapsSDR DHL2002720513Skin · corrodedDURING "C" CHECK, CORROSION ON FUSELAGE SKIN AT B.S. 357-360 STR 22L. REPAIRED IAW SRM.Oct 5, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720510Skin · gougedDURING C CHECK DISCREPANCY AS FOLLOWS, GOUGE IN FUSELAGE SKIN AT B.S. 670, ABOVE STR 26R. REPAIRED IAW SRM.Oct 5, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002720500Skin · gougedDURING "C" CHECK, FOUND GOUGE IN FUSELAGE SKIN AT BS 630, BELOW STR 24R. CUTOUT DAMAGED AREA. FABRICATED DOUBLER IAW B727 SRM 53-30-3 FIG 1. INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 1.Oct 5, 2002 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002726004Valve · failedANTI-ICE DUCT OVERHEAT LIGHT ILLUMINATED AT TAKE-OFF. APPEARS TO BE NR 3 ENGINE. REMOVED & REPLACED NR 3 WING ANTI-ICE VALVE. OPS CHECKED IAW B727 M/M 30-11-31. OPS CHECKED GOOD. REJECTED TAKE-OFF! TAKE-OFF WEIGHT - 144,000 LBS, AIRSPEED - 40 KNOTS, TEMPEROct 1, 2002 · N726DH · Boeing 727228 · Airfoil Anti/De-ice SystemSDR DHL2002727010Light1) MAIN ENTRY EMERGENCY EXIT LT. INOP. 2) REMOVED AND REPLACED LT. ASSY PER B-727 M/M 33-50-101. OP CHECKS GOOD.Sep 9, 2002 · N727DH · Boeing 727228 · Emergency LightingSDR DHL2002720004Power Unit1) APU FIRE WARNING SYSTEM WILL NOT TEST ON PREFLIGHT. 2) DEFERRED APU FIRE WARNING PER MEL 26-11 CAT. "C" DMI #10316 ASSIGNED. PLACARD INSTALLED.3) REF. DMI #10316 APU FIRE WARNING SYSTEM WILL NOT TEST. 4) REMOVED AND REPLACED APU OPERATING POWER UNIT. RESep 6, 2002 · N720DH · Boeing 727228 · Overheat DetectionSDR DHL2002721008Switch · out of adjustMAIN CARGO DOOR WARNING LIGHT S/O PANEL AND RIGHT AT ENTRY DOOR ILLUMINATED AT FL285 CABIN PSI WAS 7.0 TO 8.0 PSI NO LOSS OF PRESSURIZATION NOTED. DHL AIRWAYS EVENT REPORT STATES AN EMERGENCY WAS DECLARED. ADJUSTED AFT JAMB DRIFT PIN SWITCH. OPS CHECKED DOOSep 5, 2002 · N721DH · Boeing 727228 · Door Warning SystemSDR DHL2002721519Switch · out of adjustDURING ACCEPTANCE FLIGHT OUT OF C-CHECK HEAVY MAINTENANCE CREW DECLARED AN EMERGENCY LANDING DUE TO MAIN CARGO DOOR WARNING LIGHT S/O PANEL AND LIGHT AT ENTRY DOOR ILLUMINATED AT FL 285 CABIN PSI WAS 7.0 TO 8.0 PSI, NO LOSS OF PRESSURIZATION. ADJUSTED AFT JAMSep 5, 2002 · N721DH · Boeing 727228 · Door Warning SystemSDR DHL2002721504Seat Track · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN, SEAT TRACK AT STA 760 IS CORRODED AT RBL 24. REMOVED CORROSION FROM CABIN SEAT TRACK AND FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS IAW B-727 SRM 53-10-1 FIG 3. REMOVED CORRODED SEAT TRACK IAW B-727 SRM 51-30-2Aug 8, 2002 · N721DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002721503Seat Track · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN SEAT TRACK BETWEEN STA 870-848, AFT FLANGE CORRODED AT LBL 24. REMOVED CORROSION FROM CABIN SEAT TRACK, BEYOND ALLOWABLE LIMITS IAW B-727 SRM 53-10-1 FIG 1. REMOVED CORRODED SEAT TRACK. FABRICATED NEW SECTION IAWAug 8, 2002 · N721DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002721516Spar · corrodedDURING C-CHECK, LT WING UPPER FRONT SPAR ATTACH TO L/E WS 140/150 CORROSION UNDERNEATH L/E SKIN. REMOVED CORROSION FROM FRONT SPAR UPPER CHORD UPPER SURFACE WS 140 TO WS 150. MAT LOSS BEYOND ALLOWABLE LIMITS. FABRICATED 2 SPAR CHORD REPAIR ANGLES. INSTALLEAug 7, 2002 · N721DH · Boeing 727228 · Wing SparSDR DHL2002721517Frame · crackedDURING C-CHECK, BS 910 FRAME CRACKED AT STR 15 RT. REMOVE FASTENERS, BS 910 FRAME STR 15 LT IAW B-727 SRM 51-30-2. CUT OFF AND REMOVED CRACKED SECTION OF STA 910 AND STR 15 LEFT TO STR 14 LEFT IAW B-727 SRM 53-10-4. FABRICATED DOUBLER ANGLE AND FILLER ANGLEAug 7, 2002 · N721DH · Boeing 727228 · Fuselage Main, FrameSDR DHL7212002515Frame · crackedDURING C-CHECK, BS 940 FRAME (LEFT) CRACKED AT AFT FLOORBEAM ATTACH FLANGE (CONFIRMED BY NDT). STOP DRILLED CRACK IAW B-727 S/B 53-190. LOCATED AND DRILLED-UP ANGLES, DOUBLERS AND RADIUS FILLERS. INSTALLED REPAIR KIT ON FRAME IAW B-727 S/B 727-53-0190.Aug 7, 2002 · N721DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002721511Fitting · crackedDURING C-CHECK, RT WING STRINGER LUG CRACKED AT RIB ATTACH WS 656. CRACK IN LUG TERMINATES AT FASTENER HOLE ON RT VENT BOX STRINGER AT RIB ATTACH WS 656 VERIFIED BY 10 X MAGNIFYING GLASS. DRILLED UP REPAIR PARTS AND INSTALLED.Aug 7, 2002 · N721DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL2002721502Frame · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, CRACK IN MAIN FRAME, STA 540, STR 24R. STOP DRILL OF CRACK IN MAIN FRAME IAW B-727 SRM 51-10-1 FIG 1. FABRICATED DOUBLER IAW B-727 SRM 52-90-1 PAGE 207-215.Aug 7, 2002 · N721DH · Boeing 727228 · Fuselage Main, Frame
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