Boeing 727-224
Service difficulty reports · 2,252
Newest first. General aviation reporting is voluntary.
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 = '727224' 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.
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 = '727224' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHL2003746506Angle · crackedDURING C-CHECK, N/R 54144 RT WING LEADING EDGE L-ANGLE IS CRACKED JUST INBOARD OF NR 4 KRUEGER FLAP AT L/E STA 130.7. NR 4 L/E FLAP REMOVED AND REINSTALLED ON NR 54306. REMOVED FASTENERS AND SUB-STRUCTURE FOR ACCESS IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED SESDR DHL2003746502Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, N/R 54096 FUSELAGE HAS (2) DENTS BETWEEN STA 1070-1090 BETWEEN STR 17L-18L. CUT-OUT 1 EACH DENT AREA DIM 1.0 X 1.0 IAW B-727 SRM 53-30-3 FIG 3. EVALUATION OF SECOND DENT IS WITHIN LIMITS BY A/Y RATIO A .039 DIVIDED BY YSDR DHL2003746501Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE HAS DENT AT STR. 21L-22L BETWEEN STA 400-420. FOUND DENT TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGE AREA DIM 1 INCH CIRCULE IAW B-727 SRM 53-30-1 FIG 1 AND 53-30-3 FIG 13. FAB DOUBLER INTESDR DHL2003746507Stiffener · crackedDURING C-CHECK, N/R 54037 RT WHEEL WELL BS 870 AND INTERSECTION TO KEEL BEAM VERTICAL STIFFENER IS CRACKED. REMOVED DAMAGED ANGLE AND INSTALLED NEW P/N 65-18636-378 PO 316031 IAW B-727 SRM 51-30-2.SDR DHL2003745011Seat · malfunctionedFIRST OFFICERS SEAT WILL NOT LOCK INTO PLACE WHEN ADJUSTED FORWARD OR AFT. REMOVED AND REPLACED F/O'S SEAT. OPS CHECKED GOOD IAW M/M 25-10.SDR DHL2003746008Indicator · inoperativeAFTER CLEARED FOR TAKEOFF NR 1 EPR GAGE DID NOT RESPOND TO THRUST LEVER MOVEMENT ALL OTHER INDICATIONS ARE NORMAL. NR 1 ENGINE EPR SYSTEM INOPERATIVE PER MEL 77-1-1 CAT. "A". DMI 13006 C/W SPECIAL REQUIREMENTS PER 77-1. AIRCRAFT OK FOR SERVICE. REF. DMI 130SDR DHL2003747509Support · crackedDURING C CHECK, UPON REMOVAL OF NR 7 SLAT ACTUATOR SUPPORT STRUCTURE FOUND O/B MOUNT CRACKED AND I/B MOUNT CHAFED. REMOVED FUEL TANK ACCESS PANEL 7615 AND 7618 IAW B-727 M.M. 28-11-21. REMOVED DAMAGED ANGLES AND INSTALLED NEW FABBED FROM BAC1503-100145 P.O.SDR DHL2003747517Intake Duct · crackedDURING C-CHECK, N/R 53639 EMP STA 1303 WEB ABOVE NR 2 ENGINE INTAKE DUCT IS CRACKED, LOWER RT CORNER. REMOVED FASTENERS FOR ACCESS PER B-727 SRM 51-30-2. STOP DRILL AT WEB STA 1303 PER SERVICE BULLETIN 727-53-0094, REV 3 HFEC PER 727 NDT PT6-51-00-00 FIG 23.SDR DHL2003747516Stringer · corrodedDURING C-CHECK, N/R 53605 IN AFT CARGO STR 27L HAS CORROSION FROM BS 950 A TO BS 1070. CUT-OUT DAMAGED SECTION OF STR 27 L FROM STA 950A PLUS 10 TO 1080 IAW B-727 SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER USING BAC1498-145 4 PIECES AT 21 INCHES, TWO EACH ATSDR DHL2003747515Skin · dentedDURING C-CHECK, N/R 53604 IN AFT CARGO FRAME BS 1050 HAS A DENT INTO THE RADIUS BELOW STR 26 L. CUT OUT DAMAGED AREA DIM 1 INCH X 1 INCH AND FABRICATED ONE DOUBLER DIMENSIONS 10 INCH X 6 INCH USING 7075-T6 .071 PO 9912380 IAW B-727 SRM 51-40-3 FIG 1. ALODINESDR DHL2003747512Skin · dentedDURING "C" CHECK, N/R 53655, CABIN INTERIOR AT BS 560 DENT AND CRACK BTW. ST. 16R-17R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREAS DIMENSIONS 1 X 1 INCH IAW B-727 SRM 51-40-3 FIG. 1. FABRICATED ANGLE REPAIR USING 7075-T6 .063SDR DHL2003747510Stiffener · crackedDURING "C" CHECK N/R 53650 LT WING LE CAVITY LE STA. 1307 VERTICAL STIFFENER IS CRACKED AT BOTTOM END (FRONT SPAR WBL 92.8. REMOVED L/H WING ACCESS PANEL 6303 TO FACILITATE SM WORK IAW B-727 M.M. 57-30-0. REMOVED LT WING FUEL TANK ACCESS 7340 TO FACILITATE SSDR DHL2003747506Frame · dentedDURING "C" CHECK IN AFT. CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS BELOW STR 26L. CUT-OUT DAMAGE AREA APROX 1 INCH FRAME 1030 STR 26 L IAW B-727 S.R.M. 51-40-3. 2) REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2. 3)SDR DHL2003747505Frame · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR FRAME AT BS 600 DENT AND CRACK BETWEEN STR 16R/17R. CUT OUT DAMAGED AREA ON FRAME DIM 1 X .75 INCH AND FABRICATED ONE DOUBLER REPAIR DIMENSIONS 9 X 7 INCHES USING 7075-T6 .063 PO 92123380 IAW B-727 SRM 51-SDR DHL2003747504Frame · gougedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR FRAME AT BS 540 HAS A GOUGE BETWEEN ST 17R/16R. BLENDED AREA FOUND WITH OUT LIMITS IAW SRM B-727 51-10-1. FABRICATED AND INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-40-3 FIG 1. TREATED AND PRIMED IAW 51-10SDR DHL2003747503Frame · gougedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR FRAME AT BS 580 SHOW GOUGE AREA BETWEEN ST 17R/16R. BLENDED AREA FOUND WITH OUT LIMITS IAW B-727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7-75 T-6 .063 DIM 7 X 6.5 INCH PO 9912495. TREATED AND PRIMED SDR DHL2003747502Frame · gougedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN INTERIOR AT BS 640 HAS GOUGE AREA BETWEEN STR 16R/17R. BLENDED DAMAGE AREA FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-40-3 FIG 1. MATERIAL LOSS 7075 T-6 .063 P/O 9912495 DIM 6 XSDR DHL2003747514Beam · crackedDURING C-CHECK, AFT PRESS BULKHEAD BS 1183 LBL 36.4 VERTICAL BEAM CRACK INDICATION WL 149 APPROX IS ABOUT 1 INCH LONG NDT, CONFIRMED. STOP DRILLED CRACK IAW B-727 SRM 51-10-1. AREA HFEC INSPECTED AND VERIFIED CRACKS END IN STOP DRILL HOLES. INSTALLED S/B RESDR DHL2003747513Stiffener · crackedDURING C-CHECK, RIGHT WHEEL WELL BS 870 AND KEEL BEAM, VERTICAL STIFFENER IS CRACKED. RUNNING FROM UNDERNEATH REINFORCE PLATE. REMOVED PNEUMATIC DUCTS RT A/C BAY AT FLOW MULTIPLIER IAW B-727 SRM 36-00-01. REMOVED STIFFENER DAMAGED IAW B-727 SRM 51-30-2, DRISDR DHL2003747508Frame · crackedDURING "C" CHECK DISCREPANCY AS FOLLOWS, "CABIN INTERIOR TOP OF WING CENTER SECTION RT FRAME AT BS 826 GUSSET ANGLE CRACKED. NDT CONFIRMED. REMOVED AND REPLACED GUSSET RT SIDE BS 826 USING P/N 69-45596SDR DHL2003747507Bulkhead · crackedDURING "C" CHECK DISCREPANCY AS FOLLOWS, "AFT. PRESS. BULKHEAD BS 1183 RBBL 36.4 VERTICAL BEAM IS CRACKED FROM INB/OUT AFT. FLANGES. STOP DRILLED CRACKS AND INSTALLED REPAIR PARTS PER S/B 727-53-0192 REV. 1, FIG. 2.SDR DHL2003747511Spar · crackedDURING "C" CHECK N/R 53401 RT. ELEVATOR REAR SPAR AT ELEVATOR STATION 99.79 HAS A CRACK IN THE LOWER RADIUS. ( VERIFIED WITH HFEC) REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0059 P/N 65C30825-24 PO 312612.SDR DHL2003747501Structure · chafedDURING C-CHECK DISCREPANCY AS FOLLOWS, DEEP CHAFE MARK ON DOUBLER OUTBOARD LEADING EDGE OF INBOARD FOREFLAP LT. REMOVED OLD DOUBLER AND FABBED NEW DOUBLER IAW B-727 SRM 57-50-4 FIG 1 FROM 2024-T3 .050 PO 9912495 2. DOUBLER DIMENSIONS 4 INCH X 4 INCH. ALODINSDR DHL2003747500Web · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN FLOOR SUPPORT WEB AT BS 870 LT SIDE OUTBOARD BY THE EMERGENCY EXIT LBL 60 IS CRACK (MKD). REMOVED FLOOR SUPPORT FOR REPAIR IAW B-727 SRM 51-30-2. CUT-OUT AREA DIM 1.5 INCH X 1 INCH AND FABRICATED ONE FILLER 1.5 INSDR DHL2003746007Fire Detector · malfunctionedNR 1 ENGINE FIRE DETECTION SYSTEM-A UNABLE TO TEST. NR 1 ENGINE OVERHEAT AND FIRE DETECTION SYSTEM-A DEFERRED PER MEL 26-6 CAT-C. DMI 12653 PLACARD INSTALLED. REF DMI 12653 1 ENGINE FIRE DETECTION SYSTEM-A UNABLE TO TEST. REMOVED AND REPLACED FIRE DETECTIOSDR DHL2003746006Windshield · crackedR2 WINDOW ARCING. COMPLETED ABNORMAL PROCEDURES. OUTER PANE CRACKED. REMOVED AND REPLACED R2 WINDOW IAW M/M 56-12-11. ADJUSTED ANTI-ICING SYSTEM PER M/M 30-41-02. OPS CHECKED GOOD. REMOVED AND REPLACED NR 2 WINDOW HEAT CONTROLLER IAW M/M 30-40-00.SDR DHL2003746005Warning Horn · inoperativeAPU FIRE WARNING HORN, IN NOSE GEAR WELL, IS INOPERATIVE. TRANSFERRED TO DMI 12489 PER MEL 26-11-2 CAT-C. REF DMI 12489 APU FIRE WARNING HORN IN NOSE GEAR WELL IS INOPERATIVE. TROUBLESHOT PER WDM 49-41-0, FOUND HORN INOPERATIVE. REMOVED AND REPLACED HORN, SDR DHL2003745010Switch · out of adjustRIGHT MAIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. ABNORMAL PROCEDURE COMPLETED. LIGHT EXTINGUISHED. PLACED RT MAIN DOOR ANNUNCIATOR ON MEL 32-1. DMI 12479 AIRCRAFT OK FOR SERVICE. REF DMI 12479 RIGHT MAIN DOOR ANUNNCIATOR INOPERATIVE. FOUND RIGHT GEAR DSDR DHL2003746004Battery · dischargedEMERGENCY EXIT LIGHT DOES NOT ILLUMINATE OVER FORWAR ENTRY DOOR DURING STANDBY POWER CHECK. REPLACED BATTERIES AND LIGHT ASSEMBLY IN ENTRYWAY IAW M/M 33-50-71. OPS CHECKED GOOD.SDR DHL2003745009Warning System · malfunctionedRED "DOORS" LIGHT AND YELLOW "RT GEAR DOOR" INTERMITTENTLY COMES ON IN FLIGHT WITH GEAR HANDLE IN THE "OFF" POSITION. RIGHT LANDING GEAR DOOR WARNING SYSTEM DEFERRED IAW MEL 32-1, DMI #12425. PLACARD INSTALLED. CAT. "C" DEFERRAL.SDR DHL2003745008Bulb · burned outNR 1 ENGINE FIRE INDICATOR LIGHT INOPERATIVE. RE-LAMPED NR 1 ENGINE FIRE INDICATOR LIGHT PER DHL B-727 M/M 26-11-03. OPS. CHECKED SATISFACTORY.SDR DHL2003745007Switch · dirtyAFTER TAKEOFF WHEN GEAR HANDLE SELECTED TO OFF, POSITION "R GEAR DOOR" LIGHT ON S/O PANEL ILLUMINATED AND RED GEAR DOOR LIGHT ON FORWARD PANEL ILLUMINATED - PERFORMED ABNORMAL PROCEDURES PER AOM, LIGHTS EXTINGUISHED. RT MLG DOOR WARNING SWITCH INSPECTED AND SDR DHL2003746003Fire Detector · will not testAPU FIRE TEST INOPERATIVE. TRANSFERRED TO DMI 12262 MEL 26-11 CAT-C. PLACARD INSTALLED. IN REF TO DMI 12262. APU FIRE TEST INOPERATIVE. REMOVED AND REPLACED APU FIRE TEST RELAY. NO HELP, DMI 12262 REMAINS OPEN.SDR DHL2003747005Annunciator · shortedAFTER DEPARTING CVG IN HEAVY RAIN, ESSENTIAL POWER WARNING LIGHT STARTED TO PARTIALLY ILLUMINATE FOLLOWED BY ALL 3 REVERSER LIGHTS, THEN GEAR LIGHTS. NO OTHER INDICATIONS OF ACTUAL PROBLEMS THOUGH. CYCLED WARNING LIGHTS TEST SWITCH TO BRIGHT AND LIGHTS WENT SDR DHL2003745006Switch1) WHEN GEAR HANDLE WAS PLACED IN OFF POSITION AFTER GEAR RETRACTION, RED DOORS LIGHT AND RT GEAR DOOR LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. DOOR LIGHT OUT. GEAR DOOR LIGHT ON SO PANEL.2) REMOVED AND REPLACED RIGHT MLG DOOR SWITCH. OPS GOOD IAW 72SDR FX72003F00001Indicator · failedDURING THE BEFORE TAKEOFF CHECK OF THE ELEVATORS, THE LEFT ELEVATOR POSITION INDICATION FAILED AIRCRAFT RETURNED TO GATE. FLIGHT MECHANIC VERIFIED CORRECT OPERATION OF ELEVATORS IAW MEL 27-10 OF THE DDPG. AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCISDR GAIA03007OPIndicator · false indicationFLT 879 - RNO-SJC - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE OIL QUANTITY ON NR 2 ENGINE WAS STEADILY DECREASING. THE CREW DECLARED AN EMERGENCY AND MADE A PRECAUTIONARY SHUT DOWN OF THE NR 2 ENGINE. DURING APPROACH THE OIL QUANTITY RETURNED TO NORMALSDR DHL2003746002Warning Light · illuminatedRTO AT 169,300 POUNDS, ZERO AIRSPEED, -2C, 720 PA IN CVG. BRAKE ENERGY NORMAL, AFTER DEICING WHILE IN POSITION ON RUN-WAY WITH 80 PERCENT N1, THE NR 1 SMOKE DETECTOR WARNING LIGHT ILLUMINATED MOMENTARILY PRIOR TO TAKEOFF. REJECTED TAKE-OFF. THE LIGHT EXTINGUSDR DHL2003747004Fire Detector1) #1 ENGINE GROUND CIRCUIT DETECTOR LIGHT ILLUMINATED.2) REMOVED AND REPLACED #1 ENGINE FIRE DETECTOR IAW 26-11-22. SYS OPS CHECKED GOOD IAW 26-11-0.SDR DHL2003746001Smoke Detector1) LOWER CARGO FIRE DETECTOR.2) FOUND CODE A14836. REMOVED AND REPLACED SMOKE DETECTOR IAW B727 M/M SUPPLEMENTAL 26-16-01. TESTED IAW B727 M/M 26-16-00. OPS CHECKED NORMAL.SDR DHL2003745005Warning System · malfunctionedFIRE WARNING BELL IS MAKING STRANGE NOISE AND NO BELL. REPLACED AURAL WARNING BOX. OPS CHECKED GOOD IAW B727 M/M 31-26-0.SDR GAIA03003OPSign · inoperativeDURING ROUTINE MAINTENANCE AT PHL, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. FOUND UNIT TO BE LOOSE. RESEATED AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR DHL2003747003Fire Detector · illuminatedFIRE PROTECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED, NR 1. PLACED ON MEL 26-9-1 DMI 11789. PLACARDS INSTALLED. REF DMI NR 11789 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. OPS CHECK NR 1 ENG FIRE DETECTOR, NO DEFECTS NOTED PER MM 26-11-001. THISSDR DHL2003747002Fire Detector · illuminatedFIRE PROTECTION DETECTOR CIRCUIT GROUND LIGHT NR 1 ILLUMINATED. TRANSFERRED NR 1 GROUND FAULT FIRE PROTECTION TO DMI 11778 IAW M/M 26-9-1. PLACARD INSTALLED.SDR DHL2003747001Fire Loop · out of positionON P6-3 CIRCUIT BREAKER PANEL NR 1 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED NR 1 GROUND FAULT DETECTION SYSTEM TO DMI 11753 IAW MEL 26-9. PLACARD INSTALLED. RE; DMI 11753 - NR 1 GROUND FAULT ILLUMINATED. REPOSITIONED FIRE LOOP THAT WAS TOUCHISDR DHL2003745004Switch1) THE RED DOORS LIGHT AND THE RIGHT GEAR DOOR LIGHT CAME ON WHEN THE LANDING GEAR HANDLE WAS MOVED TO OFF AFTER GEAR RETRACTION. THE LIGHTS WENT OUT WHEN THE GEAR HANDLE WAS MOVED TO UP. SEE LOG PAGES 323267 AND 323259.2) DEFERRED RIGHT GEAR DOOR INDICATIONSDR DHL2003745003Switch · dirtyAFTER GEAR RETRACTION UPON MOVING GEAR HANDLE FROM UP TO OFF POSITION. S/O RT GEAR DOOR LIGHT ILLUMINATED, AND FRONT PANEL DOOR LIGHT ILLUMINATED. BROUGHT LEVER BACK TO UP AND ALL DOOR LIGHTS EXTINGUISHED. TROUBLESHOT SYSTEM, FOUND DEBRIS AT RT MLG WARNING SDR DHL2003745002Switch · malfunctionedAFTER DEPARTURE IN STL WHEN GEAR HANDLE WAS MOVED FROM UP TO OFF RT GEAR DOOR ON ANNUNCIATOR PANEL ILLUMINATED, AND DOOR LIGHT ON PILOTS PANEL ILLUMINATED. GEAR HANDLE THEN MOVED BACK TO UP AND LIGHTS EXTINGUISHED. GEAR HANDLE REPOSITIONED BACK TO OFF AND NOSDR DHL2003745001Indicator1) IN-FLIGHT SHUTDOWN ENGINE #3, OIL TEMPERATURE GAUGE PEGGED ABOVE 165 DEGREE (SUSPECT GAUGE).2) REMOVED AND REPLACED FAULTY OIL TEMPERATURE INDICATOR. OPS CHECKED GOOD. WORK DONE IAW M/M 79-34-0.SDR DHL2002745016Line · contaminatedTAKEOFF REJECTED DUE TO SLOW RESPONDING EPR GAGE ON ENGINE NR 3. TAKE OFF WT. = 137.8, PRESSURE ALTITUDE = 900, OAT = + 8 C, WIND 120 AT 6 KTS. DEFERRED PER MEL 77. CONTROL 11422. ABORT IAS 80 KTS. BRAKE ENERGY ZONE = NORMAL. ALL OTHER ENGINE INDICATIONS
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