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 DHL2002747014Warning Light · illuminatedNR 1 ENGINE FIRE DETECTION GROUND FAULT LIGHT ILLUMINATED. DEFERRED IAW MEL 26-9 CONTROL 11371 ASSIGNED.SDR DHL2002747013Pin1) #1 ENGINE GROUND FAULT LIGHT ILLUMINATED 45 MIN. AFTER POWER ON. TROUBLESHOT SYSTEM - WITH FORWARD CONNECTOR REMOVED LIGHT STILL REMAINS ON - REINSTALLED CONNECTOR - PROBLEM IS WITH WIRING TO CONNECTOR.2) DEFERRED PER MEL 26-9-1 CAT. "C". DMI #11339 PLASDR DHL2002745015Connector · dirtyAFTER TAKE OFF PLACED GEAR HANDLE UP, ALL LIGHTS WENT OFF NORMALLY. WHEN GEAR HANDLE WAS PLACED TO OFF, RED DOOR LIGHT CAME ON FORWARD PANEL, AND RED GEAR DOOR LIGHT ON S10 PANEL CAME ON. PLACED GEAR HANDLE BACK TO UP, AND ALL LIGHTS WENT OFF. GEAR HANDLE BACSDR DHL2002747012Warning Light · illuminatedNR 1 ENGINE GROUND CIRCUIT DETECTOR LIGHT ILLUMINATED. DEFERRED PER MEL 26-9. CONTROL 11286 ASSIGNED. PLACARD INSTALLED.SDR DHL2002747011Element · out of positionENGINE NR 1 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. DEFERRED IAW MEL 26-9. ASSIGNED CONTROL 11265. PLACARD INSTALLED. REF. DMI 11265 ENGINE NR 1 DETECTOR CIRCUIT LIGHT ILLUMINATED. REPOSITIONED NR 1 ENGINE FIRE DETECTOR ELEMENT, CLEANED & RESEATED SDR DHL2002747010Warning Light · illuminatedNR 1 ENGINE FIRE WARNING GROUND FAULT SYSTEM LIGHT ILLUMINATED. DEFERRED PER MEL 26-9, CONTROL 11203, PLACARD INSTALLED.SDR DHL2002747009Warning Light · illuminatedON PREDEPARTURE CHECK, NR 1 ENGINE DETECTOR GROUND FAULT LIGHT ILLUMINATED ON CIRCUIT BREAKER PANEL P6-3. CLEANED CONNECTORS AT THE RESPONDER AND THE TAIL CONNECTOR WITH NO JOY. RESECURED ALL CLIPS ON THE DETECTOR ELEMENTS AND GROUND FAULT LIGHT WENT OUT. SDR DHL2002747008Terminal1) ENGINE NO.1 DETECTOR CIRCUIT GROUND LIGHT ON CIRCUIT BREAKER PANEL P6-3 ILLUMINATED INTERMITTENTLY. FIRE DETECTION TESTED OK.2) FOUND WIRE 458-20 PULLED OUT OF TERMINAL CONNECTOR. INSTALLED NEW TERMINAL CONNECTOR. OPS CHECKED SERVICEABLE.SDR DHL2002745014Light · inoperativeFLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. OPS CHECKED PORTABLE EMERGENCY LIGHTS IAW DHL B727 M/M 33-50-101. OPS CHECKED GOOD.SDR DHL2002746011Battery · dischargedLOWER CARGO FIRE DETECTION FORWARD CARGO INOPERATIVE. TROUBLESHOT AND FOUND SENSORS F15137 AND F15856 LOW BATTERIES. REMOVED AND REPLACED BATTERIES. GROUND OPS CHECKED NORMAL IAW B727 SUPPLEMENTAL M/M 26-16-01.SDR DHL2002746010Blade · out of adjustFIRST OFFICER'S WIPER IS INOPERATIVE. FIRST OFFICER'S WIPER BLADE TENSION HIGH. WIPER ARM PRESSURE ADJUSTED PER MM 30-42-42. TESTED SERVICABLE.SDR DHL2002746009Light · looseEMERGENCY EXIT LIGHT ASSEMBLY LOOSE, FALLS OUT. RESECURED EMERGENCY EXIT LIGHT IAW MM 33-50-00. OPS CHECKED NORMAL.SDR DHL2002745013Battery · dischargedEMERGENCY EXIT LIGHT AT AIRCRAFT ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHT. OPS CHECKED GOOD IAW B727 MM 33-50-00.SDR DHL2002746008Bleed Valve · malfunctionedNR 3 ENGINE COMPRESSOR. REJECTED TAKEOFF. WOULD NOT MAKE T/O THRUST AND WAS COMPRESSOR STALLING. REPLACED NR 3 ENGINE PRBC VALVE PER M/M 75 -30-1. GROUND RAN PER DHL JRH SATISFACTORY. WT. 127.7, IAS 60 KTS, 15 DEGREES OAT, 1150 PRESS ALT.SDR DHL2002745012Switch · out of adjustNOSE GEAR DOORS LIGHT ILLUMINATED IN FLIGHT. ADJUSTED RT NOSE GEAR DOOR SWITCH IAW DHL B727 M/M 32-62-11. OPS CHECKED GOOD.SDR DHL2002745011Detector · shortedNR 1 ENGINE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. EXTINGUISHES AT 10,000 FT AND DIMMER WITH THRUST AT IDLE. DEFERRED NR 1 GROUND DETECTOR PER MEL REF. 26-9-1, PLACARD INSTALLED CONTROL 10655. WORKING DMI 10655 - NR 1 ENGINE DETECTOR CIRCUITSDR DHL2002745010Connector · dirtyNR 1 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED & CLEANED CONNECTOR PLUG. OPS CHECKED GOOD IAW M/M 26-11-00.SDR DHL2002747006Solenoid Valve1) IN FLIGHT, HYDRAULIC SYSTEM "A" DECREASED TO 0.2. ENGINE #1 LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY. PERFORMED ABNORMAL PROCEDURES. "A" HYDRAULIC SYSTEM FLUID SHUTOFF SWITCHED CLOSED FOR 7 MINUTES. (NOTE: DHL INSPECTION AND SURVEILLANCE REPORT DATED SDR 2002F01029Ballast · malfunctionedDURING CLIMB, SMOKE ALARMS IN BOTH AFT LAVATORIES WENT ON, SMOKE WAS NOTICED. AFTER 20 OR 3 MINUTES IT WAS CLEAR, AFT GALLEY POWER WAS SWITCHED OFF AS PRECAUTIONARY A/C CONTINUED TO MIAMI. ON THE GROUND, FOUND AFT CABIN CEILING LIGHTS DUAL FILTER BALLAST BURSDR DHL2002745009Warning System · malfunctionedNR 2 ENG FIRE WARNING WILL NOT TEST IN COCKPIT. PERFORMED OPS CHECK OF NR 2 ENGINE FIRE WARNING, OPS GOOD IAW 26-11-001.SDR GAIA02132OPEngine · malfunctionedFLT 2834 - PHL-CLT - DURING APPROACH TO CLT, THE CREW NOTICED THE NR 1 ENGINE OIL QUANTITY DECREASING. THE CREW DECIDED TO MAKE A PRECAUTIONARY SHUTDOWN OF THE ENGINE AND DECLARE AN EMERGENCY. AN UNEVENTFUL LANDING WAS MADE. THE AIRCRAFT WAS MAINTENANCE FERSDR GAIA02100STHinge · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION PER AEI SERVICES BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02093STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL RIGHT MAIN CARGO COMPARTMENT BS 600. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1, FABRICATED REPAIR DOUBLER IAW B727 SRM 51-40-3 AND 53-10SDR GAIA02101STHinge · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE AFT MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION AEI SERVICE BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02081STDoor Frame · corrodedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT AT THE E/E ACCESS, THE AFT DOOR LOCKING FRAME HAD CORROSION AT THE FRAME TO SKIN AT BS 460, STRINGER S29L TO S28L. REMOVED FRAME DAMAGE, AND REPAIRED PER BOEING SRM 51-10-2 FIGURE 3. THE AIRCRAFT WAS RETURNSDR GAIA02083STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE EXTERIOR NOSE SECTION AT BS 310 THROUGH 330 BETWEEN STRINGERS 21R TO STRINGER 22R SKIN WAS DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER TREATED AND PRIMED AREA IAW SRM 53-30-3 FISDR GAIA02085STStringer · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE MAIN CARGO COMPARTMENT INTERIOR AT BS 720B HAD A CRACK AT STRINGER S15L FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED NEW PART IAW B727 SRM 53-10-3, FIG 5. THE AIRCRAFT WAS RETURNEDSDR GAIA02086STStringer · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO COMPARTMENT INTERIOR BS 720B HAD A CRACK AT STRINGER S15R END, FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW PART IAW B727 SRM 53-10-3, FIGURE 5. THE AIRCRASDR GAIA02091STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT SIDE MAIN CARGO COMPARTMENT BS 560. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727-SRM 51-40-3, FSDR GAIA02092STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT MAIN CARGO COMPARTMENT BS 580. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3 AND 53-SDR GAIA02090STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME DENTED JUST ABOVE FLOOR LEVEL RIGHT CABIN BS 540. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 2. THESDR GAIA02089STFrame · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE BS 360, FRAME INBOARD FLANGE WAS DENTED AND CRACKED IN THE AREA OF STRINGER 16 LEFT. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-3, FIG 1 FABRICATED DOUBLER IAW B727 SRM 51-20-1 AND 51-40-3 FIG 1. THE AIRCASDR GAIA02088STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD CARGO COMPARTMENT, THE FRAME AT BS 680 HAS THREE DENTS INTO THE RADIUS OF STRINGERS S25L TO S23L. COLD WORKED DENTS, NDT FOUND NO CRACKS, FABRICATED DOUBLER REPAIR IAW B727 SRNM 51-40-3, FIGURE 1SDR GAIA02087STPlenum · corrodedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT PLENUM LOWER SKIN HAS CORROSION IN TWO PLACES. FOUND CORROSION OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW B727 SRM 57-30-3 FIGURE 8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02084STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1130, STRINGER 27L. REMOVED OLD REPAIR CUT OUT DAMAGED AREA INSTALLED FILLER, DOUBLER AND TRIPLER PER BOEING SRM 53-30-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. SDR GAIA02082STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1090, STRINGER S15R. CUT OUT DAMAGED AREA FABRICATED DOUBLER IAW B727 SRM 53-30-3, FIGURE 1, SHEET 2, PATE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02080STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD LOWER CARGO DOOR CUTOUT FRAME AND SKIN WAS DENTED NEAR STRINGER S23R AT THE FORWARD PORTION OF THE DOOR CUTOUT FRAME (FUSELAGE SKIN). C/A: ACCOMPLISHED REPAIR IAW REPAIR ORDER. AIRCRAFT WAS RETSDR DHL2002747005Light · inoperativeENGINE NR 1 FIRE BOTTLE DISCHARGE BUTTON IS NOT ILLUMINATED DURING TEST. RELAMPED NR 1 ENGINE FIRE BOTTLE DISCHARGE BUTTON, OPS CHECK GOOD IAW 727 M/M 33-10-00.SDR DHL2002745007Warning System · malfunctionedAT KSAN T/O WARNING HORN SOUNDED WHEN THRUST ADVANCED FOR T/O. T/O ABORTED. CYCLED CONTROL SURFACES AND STAB TRIM INDIVIDUALLY. NO HORN AFTER SPEED BRAKE WAS CYCLED. THEN OPS NORMAL. DEPARTURE UNEVENTFUL. OPS CHECK T/O WARNING PER 31-26-00. OPS CHECK SASDR GAIA02074OPLight · will not testDURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE LEFT FORWARD ENTRY DOOR, EMEREGNCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR DHL2002745005Switch · dirtyRTO AT PHX DUE TO TAKEOFF WARNING HORN. EVERYTHING SET PROPERLY. CLEANED AND RAN STAB TRIM LIMIT SWITCHES PERFORMED A SATISFACTORY TAKEOFF WARNING TEST MM 27-40-61.SDR 2002F00797Sensor · faultyOUT OF SVMC AFTER TAKEOFF WITH LANDING GEAR LEVER IN UP POSITION AND FLAPS FROM 5 DEGREES TO 2 DEGREES THE TAKEOFF WARNING HORN STARTED TO SOUND, ACCOMPLISHED AIR GROUND SENSOR PROCEDURES AND AIRCRAFT RETURNED TO SVMC. THE LEFT GROUND AIR SENSOR WAS REPLACED SDR DHL2002746007Connector · brokenON PERFORMING FURTHER MX CONCERNING ITEM 1P LOG PAGE 270926 FOUND NR 3 ENG FIRE LOOP BROKEN FROM WIRING HARNESS. REPLACED CONNECTOR IAW DHL B-727 M/M 20-11-11. NR 3 ENG FIRE WARNING CHECKS GOOD IAW B-727 M/M 26-11-00.SDR DHL2002745502Skin · corrodedDURING C-CHECK, LT WING LWR WING SKIN AT STR 9 FROM WING STA 519 TO STA 421.50 IS CORRODED. REMOVED CORROSION ON LT WING LWR IN SPAR SKIN, FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B-727 SRM 57-30-1 FIG 1. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DWG FSDR FX72002F00000Jackscrew · inoperativeWHILE DOING (C) CHECK, ROUTINE CARD 65-C-1 FOUND METAL SHAVINGS IN AUX BRAKE CAVITY. REMOVED AND REPLACED STABILIZER JACKSCREW PER MM. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR DHL2002745505Stiffener · crackedDURING C-CHECK, AFT PRESS BULKHEAD BS 1183 VERTICAL BEAM LBL 36 CRACKED WL 250 APPROX (NDT CONFIRMED). STOP DRILLED CRACK ON PRESSURE BULKHEAD BEAM IAW B-727 SRM 51-10-1. INSTALLED KIT 65C344406-13 REPAIR MOD IAW B-727 S/B 53-192.SDR DHL2002745504Shear Tie · corrodedDURING C-CHECK, IN FWD CARGO SHEAR TIE HAS CORROSION AT BS 720R STR 28R. DAMAGE BEYOND LIMITS IAW B-727 SRM 53-10-1 AND 51-10-1. FABRICATED REPAIR IAW B-727 SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE REPAIR IAW B-727 SRM 53-10-4 FIG 15.SDR DHL2002745503Stiffener · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, AFT PRESS BULKHEAD BS 1183 VERTICAL BEAM LBL 17.81 CRACKED AT FWD FLANGE PASSING RADIOS TO LATERAL SIDE WL 273 (NDT FINDING). REMOVED AND REPLACED FRAME IAW B-727 S/B 53-210. INSTALLED PREVENT MOD IAW B-727 S/B 53-210.SDR DHL2002745501Fitting · crackedDuring C Check "Discrepancy"- R/H Wing rear spar O/B attach fitting crackecked ( Gear beam attach fitting).1) Removed R/Wing R/spar O/B attach fitting for main gear beam I.A.W. B-727 S/B 57-167 R2.2) Drilled-up new replacement fitting P/N 65-16289-12 per B-727SDR GAIA02067OPTire · rupturedDURING TAKE OFF ROLL, CREW FELT A BUMP. WHILE ON ROUTE COMPANY OPERATIONS NOTIFIED CREW THEY HAD BLOWN THE NR 3 TIRE. CREW ELECTED TO CONTINUE ON ROUTE. CREW DUMPED FUEL AND DECLARED AN EMERGENCY LANDING. LANDING WENT UNEVENTFUL. AFTER POST FLIGHT IT WAS
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