Boeing 727-22C
Service difficulty reports · 2,328
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 = '72722C' 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 = '72722C' 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 DHL95706001Engine · failedDURING DEPARTURE, EXPERIENCED MODERATE AIRFRAME VIBRATION. RETARDED NR 1 THUST LEVER BELOW 75 PERCENT N1, VIBRATION STOPPED. DURING CRUISE, VIBRATION APPEARED AT 90 PERCENT N1. JETTISONED FUEL, PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. REMOVED AND RSDR UPS203281Eel Battery · dischargedMAINTENANCE REPORTED EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN SWITCHED TO ON. REPLACED EMERGENCY EXIT LIGHT BATTERY, OPS CK NORMAL.SDR UPS203213Eel Assy · malfunctionedMAINTENANCE REPORTED EMER EXIT LIGHT OVER FWD ENTRY DOOR, WHEN TURNED ON COMES ON BRIGHT FOR APPROX 45 SECONDS THEN GOES DIM. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECK NORMAL.SDR 95FDEA00446Engine · failedDURING FLT HAD NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT WITH 46 PSI OIL PRESS NR 1 ENG SHUTDOWN AS PER RED TABS. LIGHT CAME ON AT START OF DESCENT. MINOR VIBRATION NOTED DURING FLIGHT, BUT ALL INDICATIONS NORMAL UNTIL LIGHT CAME ON. FOUND METAL IN THE OIL SYSSDR 95ZZZW647Actuator · failedLOST 'A' SYSTEM HYDRAULICS INFLIGHT, LANDED IN MCI WITHOUT FURTHER INCIDENT. FOUND THE NR 2 FLAP ACTUATOR SEAL RUPTURED. REPLACED THE NR 2 FLAP ACTUATOR.SDR 95ZZZX1937Line · crackedLOST A-SYSTEM HYDRAULICS IN-FLIGHT, ACCOMPLISHED MANUAL GEAR EXTENSION AND LANDED IN SAT WITHOUT FURTHER INCIDENT. FOUND NR 2 SPOILER RETURN LINE CRACKED. REPLACED LINE, A-SYSTEM FILTERS AND THE A-SYSTEM ENGINE PUMPS.SDR UPS202839Shear Web · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON TWO HOLES THROUGH LT SHEAR WEB AT BS 1140 TO 1145, LBL 30, AS SEEN FROM BELOW. INSTALLED REPAIR PER SRM 51-40-2 AND 51-30-2.SDR UPS202838Seat Track · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK LWR FLANGE OF CHORD, STA 760, LBL 45. INSTALLED REPAIR PER SRM 53-10-2, 51-30-2, 51-10-6, AND BOEING DRWNG 65-34144-13.SDR UPS202837Sill · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL WEB, UNDER DOOR FITTING, STA 580. INSTALLED REPAIR PER USRM 51-40-2.SDR UPS202836Fitting · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM TO SEAT TRACK SUPPORT FITTING, BS 760, LBL 48. REPLACED PER SRM 51-40-4 AND 51-30-2.SDR UPS202835Floorbeam · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR PANEL BEAM WEB, BS 760, LBL 48, BELOW FLOOR LEVEL AFT SIDE. INSTALLED REPAIR PER SRM 51-40-2.SDR UPS202834Rib · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON O/B RIB STA 1365, LT SIDE. INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.SDR UPS202833Rib · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON O/B RIB STA 1365, RT SIDE. INSTALLED REPAIR PER SRM 51-40-3 AND 1-30-2.SDR UPS202832Web · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FIREWALL WEB AT BS 1342, LBL 24, WL 220. INSTALLED REPAIR PER SRM 51-40-2 AND 54-10-3.SDR UPS202831Shear Tie · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON SHEAR TIE BS 1323, BETWEEN STRINGERS 17 AND 18L. REPLACED PER SRM 51-40-3 AND 53-10-2.SDR UPS202830Channel · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT CHANNEL STA 1342, WL 247, RBL 18. REPLACED PER UPS EO 727-5530-4601.SDR UPS202829Frame · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT CHANNEL, AFT SIDE OF FRAME, STA 1342, WL 247, LBL 18. REPLACED PER UPS EO 727-5530-4601.SDR UPS202828Frame · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT LWR FRAME CHORD STA 1342, LBL 24, WL 220. REPLACED PER UPS EO 727-5530-4601.SDR UPS202827Frame · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT LWR FRAME CHORD STA 1342, RBL 24, WL 220. REPLACED PER UPS EO 727-5530-4601.SDR UPS202826Chord · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE 1342 CHORD FWD SIDE. REPLACED PER UPS EO 727-5530-4601B.SDR UPS202825Chord · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL, STA 1342. REPLACED PER UPS EO 727-5530-4601B.SDR UPS202824Chord · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT O/B CHORD, STA 1342, LBL 30, WL 250. REPLACED PER UPS EO 727-5530-4601.SDR UPS202823Chord · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT O/B CHORD, STA 1342, RBL 30, WL 250. REPLACED PER UPS EO 727-5530-4601.SDR UPS202822Frame · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT FRAME CHORD, STA 1342, RBL 20, WL 238. REPLACED PER UPS EO 727-5530-4601.SDR UPS202821Frame · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT FRAME CHORD, STA 1342, LBL 20, WL 238. REPLACED PER UPS EO 727-5530-4601.SDR UPS202817Rib · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON RT UPPER RIB CHORD AT RBL 70.5, BS 760, FORWARD TWO FASTENER HOLES. INSTALLED REPAIR PER UPS EO B727-5710-1271F.SDR UPS202787Wedge · delaminatedDURING 'C' CHECK, MAINTENANCE FOUND LT AILERON O/B TRAILING EDGE WEDGE IS DELAMINATED. REPLACED WEDGE PER SRM 51-80-6, 51-10-2, 51-30-2, MM 27-10-41.SDR UPS202771Fitting · crackedDURING 'C' CHECK, MAINTENANCE FOUND MAIN CARGO DOOR LATCH SUPPORT FITTINGS IN THE FUSELAGE STRUCTURE CRACKED AT BS 500. REPLACED FITTING PER UPS EO B727-5310-0437.SDR UPS202770Door Frame · crackedDURING 'C' CHECK, MAINTENANCE FOUND MAIN CARGO DOOR AFT SIDE FRAME CRACKED AT DRIFT PIN RECEPTACLE AT I/B RADIUS. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-2, 51-40-3, 51-10-2.SDR UPS202769Core · damagedDURING 'C' CHECK, MAINTENANCE FOUND RT WING I/B AFT FLAP CORE WATER DAMAGED. REPLACED FLAP PER MM 27-51-02.SDR UPS202767Rib · crackedDURING 'C' CHECK, MAINTENANCE FOUND NR 5 SLAT RIB CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-50-3.SDR UPS202766Attach Points · corrodedDURING 'C' CHECK, MAINTENANCE FOUND NR 6 K-FLAP ATTACH POINTS CORRODED ON K-FLAP SIDE. REPLACED FLAP PER MM 27-81-01.SDR UPS202765Angle · corrodedDURING 'C' CHECK, MAINTENANCE FOUND NOSE LANDING GEAR LOWER LT ANGLE CORRODED. REPLACED CHORD PER SRM 51-30-2, 51-50-1, 51-40-2.SDR UPS202705Skin · delaminatedDURING 'C' CHECK MAINTENANCE FOUND LT I/B AFT FLAP TRAILING EDGE IS DELAMINATED ON TRAILING EDGE. REPLACED FLAP PER MM 27-51-02.SDR UPS202761Aileron · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND I/B AILERON CONTROL ROD FITTING CORRODED AROUND BOLT HOLE. REPLACED AILERON PER MM 27-10-11.SDR UPS202760Wedge · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND TRAILING EDGE WEDGE ON RT I/B MID FLAP CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2 AND OHM 20-50-01.SDR UPS202759Flap · corrosionWHILE IN 'C' CHECK MAINTENANCE FOUND NR 3 K-FLAP O/B HINGE O/B LUG UPPER AND LOWER BOLT HOLES HAVE PITTING AROUND O/B SIDE. REPLACED K-FLAP PER MM 27-81-00.SDR UPS202758Flap · corrosionWHILE IN 'C' CHECK MAINTENANCE FOUND NR 6 K-FLAP O/B HINGE LUG ATTACH POINT HAS CORROSION UNDER TOP BOLT O/B SIDE. REPLACED K-FLAP PER SRM 57-51-1 AND MM 27-81-01.SDR UPS202757Skin · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL SKIN AT BS 259.7-277. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3, 51-30-5, 51-20-21, 51-30-2.SDR UPS802707Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B AILERON TAB, TRAILING EDGE. INSTALLED REPAIR PER SRM 51-80-3 AND 51-40-6.SDR UPS802706Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B, MID FLAP TRAILING EDGE WEDGE, I/B END, UPPER SURFACE. INSTALLED REPAIR PER SRM 51-40-6.SDR UPS802705Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B, AFT FLAP TRAILING EDGE. NORDERED NEW FLAP ASSY.SDR UPS802704Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT I/B AILERON TAB, T/E LWR SURFACE. INSTALLED REPAIR PER SRM 51-40-6, 51-80-3.SDR UPS802703Floor · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON WALKWAY PANEL AT STA 294.5-312, RBL 25, WL 169. REPLACED PER SRM 51-40-2, 53-10-2, 51-10-2, MM 51-20-151, AND 51-30-2.SDR CA950320101Switches · intermittent(CAN) ON APPROACH GEAR SELECTED DOWN THREE GREEN LIGHT ON. SHORTLY AFTER NOSE GEAR DOWN LIGHT INDICATOR WENT OUT. GEAR CYCLED ALL INDICATIONS NORMAL AND AIRCRAFT LANDED. NOSE GEAR POSITION AND LOCK SWITCHES REPLACED.SDR 96ZZZX1317Angle · corrodedDURING D-CHECK, INSIDE VERTICAL FIN THROUGH ACCESS PANEL 9504, CORROSION ON HORIZONTAL LEG OF HORIZONTAL L-ANGLE (CHORD) APPROXIMATELY FS 1343, LEFT SIDE. INSTALLED REPAIR S/S 301 1/2 HARD ANGLE PER SRM 51-40-4 AND 51-30-2, 6 INCH BY 10 INCH, .125 INCH. TAT:SDR 96ZZZX1316Fairing · crackedDURING D-CHECK, FAIRING NR 3329 HAS A 2 INCH CRACK IN THE END RADIUS. STOP DRILLED AT ENDS OF CRACK. ROUNDED OUT CRACK. FABRICATED DOUBLER 2024-T3.040, 4 INCH BY 4 INCH. INSTALLED DOUBLER PER SRM 51-10-1, 51-10-2 AND 51-40-3. TAT: 53,881.4 HRS. TAC: 3SDR 96ZZZX1315Seat Track · corrodedDURING D-CHECK, CORROSION ON FLOOR BEAM SEAT TRACK NR 7 APPROXIMATELY RBL 60 BETWEEN BS 700 AND BS 740, BOTTOM SIDE. CORROSION BEYOND LIMITS, REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK PER SRM 53-10-5 AND SRM 51-10-1, 44 INCHES LONG. TAT: 53,881.4 HRS.SDR 96ZZZX1314Skin · gougedDURING D-CHECK, FUSELAGE EXTERIOR, RT GALLEY SERVICE DOOR EXTERIOR SKIN CORRODED AND GOUGED JUST FORWARD OF DOOR WINDOW AT FS 650. INSTALLED EXTERNAL REPAIR PER SRM 52-00-3, FIGURE 3. TAT: 53,881.4. TAC: 36,380.SDR 96ZZZX1313Skin · corrosionDURING D-CHECK, FUSELAGE EXTERIOR, EVIDENCE OF CORROSION AT FS 360 AT LAP SEAM STR 10R. REMOVED FASTENERS PER SRM 51-30-2, CLEANED CORROSION PER SRM 51-10-6, ALODINE AND PRIMED PER SRM 51-10-2, AND REINSTALLED FASTENERS PER SRM 51-30-2. TAT: 53,881.4 HRS.
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