Boeing 727-25C
Service difficulty reports · 2,007
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 = '72725C' 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 = '72725C' 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 UPS04242854Skin · delaminatedINSPECTION TYPE: C, RIGHT WING O/B AFT FLAP HONEYCOMB FILLER DELAMINATED AT I/B END. AFT FLAP FITTINGS REMOVED FROM UNSERVICEABLE FLAP AND FITTED TO REPLACEMENT AFT FLAP IAW OHM 20-50-01 AND OHM 57-52-11. FLAP ASSY REPLACED IAW MM 27-51-12 AFT FLAP ADJUSTED SDR UPS04242760Web · crackedINSPECTION TYPE:C, CENTER ENGINE SUPPORT STRUCTURE, WEB CRACKED ON RT SIDE AT BS 1387. WEB REMOVED IAW SRM 51-30-02. WEB FABRICATED PER DRAWING 65-17555. WEB INSTALLED PER DRAWING 65-17555.SDR UPS04242861Yoke · malfunctionedINSPECTION TYPE: C, PERFORM A GVI OF CAPT & F/O CONTROL YOKES & ATTACHED LINKAGE, PAYING ATTENTION TO CORROSION, BINDING OR LOOSENESS OF BEARINGS. ROTATE EACH CONTROL WHEEL FULL TRAVEL LEFT & RIGHT CHECKING FOR ANY STIFFENESS, BINDING OR RATCHETING OF MOVEMENSDR UPS04242852Skin · crackedINSPECTION TYPE: C, CRACK ON I/B MID FLAP LOWER T/E SKIN AT I/B AFT FLAP ACTUATING ROD CUTOUT O/B AFT CORNER (LT). HFEC CONFIRMED CRACK AND MARKED END. DAMAGED AREA TRIMMED OUT IAW SRM 51-10-1. REPAIR CARRIED OUT IAW AAAE EO 2004-068-006.SDR UPS04242738Web · crackedINSPECTION TYPE:C, CRACK EVIDENT AT LIGHTENING HOLE IN THE AFT ENTRY STAIRS AREA. CRACK LOCATED AT B-STA 1263 APPROX, LEFT SIDE OF TORQUE BOX VERTICAL WEB JUST OUTSIDE DOUBLER OF PREVIOUS REPAIR. CRACK STOP DRILLED PER SRM 51-10-1. HFEC INSPECTION CARRIED OSDR UPS04242839Skin · debondedINSPECTION TYPE:C, LEFT I/B AILERON TAB DISBOND AT AFT I/B CORNER O/B END. AILERON TAB REPAIRED IAW SRM 51-40-20.SDR UPS04242774Longeron · crackedINSPECTION TYPE:C, ENGINE NR 2 LT FWD COWL UPPER LONGERON IS CRACKED AT ALIGNMENT PLATE. REMOVED LT FWD COWL UPPER LONGERON IAW SRM 51-30-02. FABRICATED NEW LONGERON PER DRAWING QF7122130-1AND SRM 54-10-06. INSTALLED NEW LONGERON IAW SRM 57-30-02.SDR UPS04242859Rod · crackedINSPECTION TYPE: C, RIGHT INBOARD AILERON TAB SUSPECT CRACK ON TAB ACTUATING ROD AT AFT END. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED. ACTUATING ROD REMOVED IAW 27-10-01. REPLACED AFT END OF ROD IAW SRM 51-30-02. REINSTALLED ACSDR UPS04242858Skin · delaminatedINSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED ON UPPER SKIN AT INBOARD END AND OUTBOARD END. AILERON TAB REMOVED IAW MM 27-10-19. DAMAGE REPAIRED IAW SRM 51-40-20, AILERON TAB REINSTALLED IAW MM 27-10-19.SDR UPS04242737Web · crackedINSPECTION TYPE: C, NR 6 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX L + R WEB CRACKED. REMOVED NR 6 KRUEGER FLAP ACTUATOR IAW MM 27-81-22. REMOVED BOTH CRACKED WEBS FOR FABRICATION IAW SRM 51-30-02. FABRICATED LT & RT WEBS AS PER DRAWING 65-16275. INSTALLESDR UPS04242736Web · crackedINSPECTION TYPE:C, NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT WEB CRACKED. REMOVED LT WEB TO FACILITATE IN FABRICATION OF NEW ONE IAW SRM 51-30- 02. FABRICATED NEW LT WEB IAW DRAWING 65-16269 AND INSTALLED ON NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPOSDR UPS04242759Angle · crackedINSPECTION TYPE:C, SUSPECT CRACK ON ANGLE ON O/B SIDE OF LOWER LEG OF BS 870 FITTING IN LT MWW. CRACK FOUND IN ANGLE, ANGLE REMOVED IAW SRM 51-30-2. NEW ANGLE FABRICATED AND FITTED IAW SRM 51-20-1, SRM 51-30-2 AND DRG 65-16330.SDR UPS04242664Intercostal · corrodedINSPECTION TYPE:C SUPPORT INTERCOSTAL FOR LWR CENTER LINE FAIRING CORRODED AT BS 740 BETWEEN S28L AND S28R. INTERCOSTAL REPLACED WITH FABRICATED INTERCOSTAL IAW SRM 51-30-02 AND 51-20-2.SDR UPS04242678Floor Support · corrodedINSPECTION TYPE: C, AFT CARGO FLOOR SUPPORT RAIL AT BS 1035 RBL 4 APPROX, CORRODED. SECTION OF FLOOR SUPPORT RAIL REPLACED IAW SRM 53-10-5 & DRAWING 65-19 388.SDR UPS04242669Angle · crackedINSPECTION TYPE: C, ANGLE CRACKED AT RT ELEPHANTS EAR. FABRICATED ANGLE IAW SRM 51-30-2, INSTALLED NEW ANGLE IAW SRM 51-20-01 FIG 7 AND BOEING DRG 65-26786.SDR UPS04242668Clip · crackedINSPECTION TYPE: C, SUPPORT CLIP FOUND CRACKED AT BS 580 BETWEEN S2L AND S3L. SUPPORT CLIP FABRICATED AND INSTALLED IAW 51-20-01 AND 51-30-2.SDR UPS04242617Web · puncturedINSPECTION TYPE: C, VENTRAL STAIRS TORQUE BOX HORIZONTAL WEB PUNCTURED AFT OF BS 1243 RIGHT O/B END. REPAIRED AREA IAW SRM 51-40-02.SDR UPS04242704Flap Track · corrodedINSPECTION TYPE:C, NR 4 FLAP TRACK, AFT PAD-B HAS CORROSION IN BORE HOLES F & G. REPAIR CARRIED OUT IAW AAAE EO 2004-061-003.SDR UPS04242702Skin Panel · corrodedINSPECTION TYPE: C, ON REMOVAL OF SKIN PANEL CORROSION FOUND ON LWR SKIN PANEL LAP JOINT S4R BETWEEN BS 615 & BS 540. REPAIR CARRIED OUT IAW AAAE 2004-061-006.SDR UPS04242675Skin · crackedINSPECTION TYPE:C, NR 6 L/E SLAT O/B UPSTOP HAS CRACK ON SURROUNDING SKIN. REPAIR CARRIED OUT IAW MM 27-81-11 & SRM 57-30-4 FIG 4.SDR UPS04242682Stringer · wornINSPECTION TYPE: C, STR WORN ON BS 1183 AFT SIDE AT WL 208 I/B OF SYS-A PRESSURE MODULE. REPAIR CARRIED OUT IAW AAAE EO 2004-061-004, UPS ENGINEERING FILE NR 727-53-20150 & SRM 51-30-02.SDR UPS04242677Bracket · crackedINSPECTION TYPE:C, NR 7 SLAT O/B TRACK TO SKIN ATTACH BRACKETS ARE CRACKED. NEW BRACKETS INSTALLED IAW SRM 51-30-02, OHM 57-51-61.SDR UPS04242676Bracket · crackedINSPECTION TYPE:C, NR 5 SLAT, O/B UPSTOP BOLT RETAINING BRACKET IS CRACKED. BRACKET REMOVED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-30-01, BRACKET INSTALLED IAW SRM 51-30-1 & MM 20-80-01. STOP ADJUSTED TO WITHIN LIMITS IAW MM 27-81-11.SDR UPS04242616Web · crackedINSPECTION TYPE: C, SUPPORT WEB BENEATH STAND-BY PUMP CRACKED AT ACCESS HOLE FOR DRAIN PLUG. STOP DRILLED CRACK AND SUPPORT WEB REPAIRED IAW SRM 51-40-2.SDR UPS04242717Skin · corrodedINSPECTION TYPE: C, SUSPECT CORROSION AT BS 640-680 S1L TO S4L. ON INVESTIGATION CORROSION FOUND INTERNALLY ON SKIN PANEL AT BS 680 - 660 S4R, BS 620 S2L - 1L, BS 540 - 530 S2L REPAIR CARRIED OUT IAW SRM 51-30-2, 33-30-01 DRAWING 65-42370, AAAE EO 2004-61-006SDR UPS04242705Skin · crackedINSPECTION TYPE: C, NR 3 LEADING EDGE FLAP ANTI ICE SKIN IS CRACKED IN TWO AREAS, ALSO LOOSE RIVETS IN ANTI ICE SKIN. REPAIRED CRACKS IAW EO B727-5750-3082. REPLACED LOOSE RIVETS IAW SRM 51-30-2.SDR UPS04242703Flap Track · corrodedINSPECTION TYPE: C, NR 4 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD-B. REPAIR CARRIED OUT IAW AAAE 2004-061-003.SDR UPS04242683Structure · crackedINSPECTION TYPE:C, NR 3 LEADING EDGE FLAP, O/B BONDING WIRE ATTACH SCREW HOLE IS CRACKED. REPAIR CARRIED OUT IAW AAAE EO 2004-061-002, UPS ENGINEERING FILE NR 727-57-20113.SDR UPS04242672Attach Fitting · crackedINSPECTION TYPE:C SUSPECT CRACK ON OFFSET GEARBOX AT ATTACHMENT LUG ON RIGHT I/B FLAPS. HFEC CONFIRMED CRACK ON LUG. OFFSET GEARBOX REPLACED IAW MM 27-51-60 PARA 1-3.SDR UPS04242715Skin · delaminatedINSPECTION TYPE: C, NR 2 SPOILER HAS DELAMINATION ON UPPER & LWR SURFACES. REPAIRED IAW SRM 51-40-5.SDR UPS04242706Skin · wornINSPECTION TYPE:C, SKIN ON LWR RUDDER L/E WORN IN SEVERAL PLACES ON LT & RT SIDES. LWR RUDDER REPLACED IAW MM 27-20-01, 27-20-11 & SRM 51-30-02.SDR UPS04242681Skin · crackedINSPECTION TYPE: C, CRACK IN SKIN FOUND AT WING SCANNING LIGHT CUTOUT LT BS 675. REPAIR CARRIED OUT IAW AAAE EO 2004-061-001, UPS ENGINEERING FILE NR 727-53-20149 & SRM 53-30-3 & MM 33-41-02.SDR UPS04242674Skin · crackedINSPECTION TYPE:C NR 6 L/E SLAT UPPER SKIN HAS SCRATCHES 2 OF WHICH ARE SUSPECT CRACKS NR 1 IS 3 INCHES O/B OF ACTUATOR, NR 2 IS 4 INCHES I/B OF ACTUATOR AND FROM PREVIOUS REPAIR CUTOUT. HFEC INSP CARRIED OUT ON THE ABOVE AREAS IAW B727 NDTM PT6 51-00-00 FIG SDR UPS04242714Yoke · crackedINSPECTION TYPE:C TAIL SKID UNIT FOUND CRACKED. TAIL SKID YOKE ASSY REPLACED IAW MM 32-71-41 & 31-71-22 FUNCTION CHECK.SDR UPS04242680Skin · damagedINSPECTION TYPE:C PULLED RIVETS & BULGE ON RT STAB LWR SKIN APPROX 4 INCHES FROM REAR SPAR AND AT STAB STA 66 APPROX. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-10-3 FIG 3, 51-10-1 & MM 51-20 -01 & 27-30-51.SDR UPS04242566Seat Track · corrodedINSPECTION TYPE:N/A ON INSPECTION SEAT TRACK SECTION FOUND CORRODED AT BS 730 AT RBBL 625 APPROX. NEW SEAT TRACK SECTION FABRICATED IAW SRM 51-20-1 AND ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW EO B727-5310-7477 STEP 28.SDR UPS04242582Bulkhead · crackedINSPECTION TYPE: C, SUSPECT CRACK IN NLG WW LOCATED ON PRESSURE WEB B STA 240 RBL 24. AREA REPAIRED IAW SRM 51-40-02.SDR UPS04242575Fairing · crackedINSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING IS CRACKED AT MID AFT END. REPLACED FAIRING IAW MM 78-30-43.SDR UPS04242590Bulkhead · crackedINSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL WALL AT LBL 24, BS 285 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2, 51-40-07 & MM 32-33-51.SDR UPS04242588Web · crackedINSPECTION TYPE: C, NOSE WHEEL WELL STRUCTURE HAS EVIDENCE OF CRACK AT BSTA 240 LBL. REPAIR CARRIED IAW SRM 51-40-02. LEAK CHECKED SATISFACTORY.SDR UPS04242584Skin · crackedINSPECTION TYPE: C, NR 6 L/E FLAP CRACKED I/B OF LANDING LIGHT & JUST ABOVE BULLNOSE. FLAP REPLACED IAW MM 27-81-01.SDR UPS04242576Panel · crackedINSPECTION TYPE: C, CRACK ON LT WING T/E PANEL UPPER SURFACE FWD OF NR 5 SPOILER. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-02 & 51-10-02.SDR UPS04242574Attach Fitting · corrodedINSPECTION TYPE: C, ATTACH FITTING AT THE BASE OF THE BS 950 STRUCTURAL FITTING HAS EVIDENCE OF INTERGRANULAR CORROSION. FITTING REPLACED IAW SRM 51-30-02 & DRAWING 65-16338.SDR UPS04242558Fitting · crackedINSPECTION TYPE: C, AREA ABOVE NR 2 HORIZONTAL FIREWALL, UPPER LEFT FITTING AT STA 1470. 5 AND WL 300.15 IS CRACKED. FITTING REMOVED IAW SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02 AND BOEING DRAWING 65-17553.SDR UPS04242557Web · crackedINSPECTION TYPE: C, LEFT I/B AILERON, O/B WEB CRACKED AT AFT UPPER FASTENER, AND FASTENER MISSING FROM WEB. REPAIR CARRIED OUT IAW 51-30-02.SDR UPS04242577Skin · corrodedINSPECTION TYPE: C, FASTENER HEAD POPPED & BULGE IN SKIN. SUSPECT CORROSION BETWEEN SKIN & STR AT BS 1065 S29L. SKIN CUTOUT BETWEEN BS 1061 AND BS 1072 AT S29L, CORROSION REMOVED IAW SRM 51-10-6. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR COMPLETED IAW AAASDR UPS04242569Skin · corrodedINSPECTION TYPE: C, DUE TO BELOW MIN EDGE DISTANCE & CORROSION ON SKIN DURING RT 740 FITTING REPLACEMENT, SKIN REPAIR REQUIRED BETWEEN S17 & S18 RT TO BETWEEN S24 & 25 RT. REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING EO 2004-054-005 & SRM 51-30-2 7 51SDR UPS04242581Skin · corrodedINSPECTION TYPE: C, BULGING IN SKIN AT BS 1183 BETWEEN S6R AND S10R. CUT OUT INTERNAL BONDED DOUBLER BETWEEN S6R TO S10R BS 1183 TO BS 1177 REFERENCE SRM 53-30-3. HFEC CARRIED OUT, NO DEFECTS FOUND. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3. REPSDR UPS04242580Angle · corrodedINSPECTION TYPE: C, CORROSION AT BS 312L VIEW IN 3RD LIGHTENING HOLE FROM FRONT OM INBOARD ANGLE MIDWAY BETWEEN UPPER AND LOWER NWW CHORDS. CORRODED ANGLE FABRICATED AND INSTALLED IAW DWG 65-18415.SDR UPS04242570Skin · crackedINSPECTION TYPE:C SUSPECT CRACK IN SKIN AT LT WING ICE LIGHT CUTOUT (UPPER FWD). REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING 2004-054-004 & SRM 51-30-02 & 51-00-00.
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