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 UPS03241247Doubler · corrodedFOUND CORROSION ON NR 3 KRUEGER FLAP EXTENDING UNDER DOUBLER REPAIR R&R REQUIRED. REMOVED AND REPLACED NR 3 KRUEGER FLAP IAW MM 27-81-01.SDR UPS03241167Battery · inoperativeFWD ENTRY DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-67, OPS CK GOOD. P/N ON 38931-002.SDR UPS03240970Check Valve · contaminatedINSPECTION TYPE:N/A AT APPROX 3000 FT CREW NOTICED SMOKE IN COCKPIT DID AN AIR TURNBACK TO DEC. REMOVED AND REPLACED THE A-SYSTEM AIR PRESUURE REGULATOR IAW M/M 2912. FOUND EVIDENCE OF HYDRAULIC FLUID IN RES AIR PRESSURE CHECK VALVE ASSY RNR ALL 3 CHECK VALVSDR UPS03240955Check Valve · leakingINSPECTION TYPE: N/A SMOKE IN COCKPIT - ATB. A/C LANDED WITHOUT INCIDENT. T/S IN PROGRESS. REMOVED AND REPLACED THE A SYS AIR PRESSURE REGULATOR IAW MM 2912. FOUND EVIDENCE OF HYD FLUID IN THE RES AIR PRESS CHECK VALVE ASSY. REMOVED AND REPLACED ALL 3 CHECSDR CA030627018Actuator · failed(CAN) 'A' SYSTEM HYDRAULIC FAILURE T/O ABORTED AND A/C RETURNED TO BLOCKS. NR 6 SLAT ACTUATOR FOUND FAILED.REPLACED ACT AND A SYSTEM PUMP CASE DRAIN FILTERS INSPECTED/REPLACED. NO CONTAMINATION FOUND. AIRCRAFT RETURNED TO SERVICE.SDR UPS03240913Skin · crackedINSPECTION TYPE: ASV, SKIN PANEL BELOW L1 AND R1 CENTER WINDOW POST HAS .375 INCH CRACK FROM EDGE TO RIVET. CONFIRMED BY DYE PENETRANT INSP. REPLACED SKIN PANEL AS PER SRM ADDENDUM EO B727-5330-5128A.SDR UPS03240690Hinge Fitting · crackedINSPECTION TYPE: C&SI, SUSPECT CRACK FOUND ON NR 5 SPOILER CENTRE HINGE FITTING HFEC INSP. CARRIED OUT ON NR 5 SPOILER CENTER HINGE FITTING IAW B727 N DTM PT 6 51-00-00 FIG 4 RESULT: CRACK CONFIRMED. CENTER HINGE FITTI NG REPLACED IAW SRM 51-30-02SDR UPS03240664Frame · corrodedINSPECTION TYPE: C&SI, FRAME ASSY ON LWR SURFACE OF APU EXHAUST PANEL ON RT WING IS CORRODED. FRAME ASSY REPLACED IAW DRAWING 6562837 & SRM 51-30-32SDR UPS03240672Support · crackedINSPECTION TYPE: C&SI, RT RAM AIR INTAKE DOOR SUPPORT BRACKET FOUND CRACKED AT BS 600 S25R. DOOR SUPPORT BRACKET FABRICATED IAW SRM 51-20-1 FIG 7, NEW BRACKET RE-PROTECTED IAW SRM 51-10-02 NEW DOOR SUPPORT AND FASTENERS RE-INSTALLED IAW SRM 51-30-02SDR UPS03240686Rib · corrodedINSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3430, FWD FORMED SECTION SUPPORT RIB HAS EVIDENCE OF HEAVY CORROSION UNDER ANCHOR NUT PLATES, JUST FWD OF GRND MOVER DOOR CUT OUT DOOR REMOVED IAW SRM 51-30-02. FRAME REMOVED IAW SRM 51-30-02. CORR OSION REMOVESDR UPS03240665Skin · crackedINSPECTION TYPE: C&SI, RT MLG DOOR, DOOR SKIN ON O/B SECTION OF DOOR ASSY CRACKED BS 910 AREA OF CRACKED SKIN TRIMMED OUT IAW SRM 52-80-02. HFEC INSP. CARRI ED OUT AROUND CUTOUT AT R/H MLG DOOR SKIN ON O/B SECTION OF DOOR ASS Y IAW B727 NDTM PT 6 510000 FIGSDR UPS03240685Door Frame · crackedINSPECTION TYPE: C&SI, SUSPECT CRACK AT NR 1 STOP FITTING CUT OUT ON FWD FRAME OF AFT CARGO DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-02 & SMRO EO 2003-025-021 UPS ENGINEERING FILE NO. B727-5330-18744-ASDR UPS03240641Angle · crackedINSPECTION TYPE: C&SI, CRACK ON ANGLE, AFT CARGO DOOR INTERIOR, ABOVE AFT DOOR STOP. REMOVED ANGLE FROM DOOR INTERIOR IAW SRM 51-30-2 FABRICATED NEW ANGL E IAW SRM 51-20-1 FIG 7 INSTALLED NEW ANGLE IAW SRM 51-30-2SDR UPS03240640Skin · crackedINSPECTION TYPE: C&SI, CRACK ON AFT CARGO DOOR INNER SKIN AT HOLE CUT OUT FOR BALANCE MECHANISM CABLE PULLEY. STOP DRILLED HOLE IAW SRM 51-10-1 REPAIR WAS THEN CARRIED OUT IAW SR M 51-40-2 REPROTECTED IAW SRM 51-10-2SDR UPS03240639Panel · erodedINSPECTION TYPE: C&SI, AIRSTAIRS COMPARTMENT, CLOSE OUT PANEL AT STA 1223 LOBE THAT JOINS TO EXTERNAL SKIN IS SHOWING SIGNS OF ERROSION ALONG ITS EDGE ON LT SIDE. AREA REPAIRED IAW SRM 51-40-3 FIG 1SDR UPS03240692Carriage · corrodedINSPECTION TYPE: C&SI, NR 6 FLAP CARRIAGE SPINDLE INTERNALLY CORRODED. NR 6 FLAP CARRIAGE REPLACED IAW OHM 57-58-02 & OHM 57-52-01 REF. TC C5 7-581-04-4D FOR INST. & DUALSDR UPS03240687Panel · contaminatedINSPECTION TYPE: C&SI, AFTER X-RAY INSP. NR 9 SPOILER FOUND TO HAVE WATER INGRESS AND CELL DISTORTATION SPOILER PANEL REPLACED IAW MM 27-61-01 & MM 27-62-01SDR UPS03240670Butt Joint · damagedINSPECTION TYPE:C&SI NDT INSP. HAS INDICATION OF MATERIAL LOSS AT BS 1080 BUTT JOINT BETW EEN S2L & 2R. VISUAL INSP. CARRIED OUT CORROSION FOUND TO EXTEND UP TO S3L NEW CUT OUT LINE MADE IAW 69-62161 S3L REPAIR CARRIED OUT IAW DRAWINGS 69-6 2161 & UPS EO B72SDR UPS03240668Frame · crackedINSPECTION TYPE: C&SI, SUSPECT CRACK ON FRAME ADJACENT TO HINGE STRUCTURE AT FWD END OF FWD CARGO BAY DOOR. ON REMOVAL OF STIFFENER IN PREPARATION FOR REPAIR A NEW CRACK WAS FO UND WHICH WAS OUTSIDE THE PERMITED REPAIR AREA. FRAME WAS REMOVED IAW SRM 51-30-0SDR UPS03240688Frame · corrodedINSPECTION TYPE: C&SI, CORROSION ON FRAME TIE ANGLE BS 351.2 S24L - S25L. DAMAGE REMOVED IAW SRM 51-10-01 FOUND OUTSIDE LIMITS. REPAIR SECTIO N FABRICATED IAW FLAP PATTERN LAYOUT AS PER SRM 51-20-1.SDR UPS03240671Floorbeam · corrodedINSPECTION TYPE: C&SI, CORROSION UNDER ANCHOR CLIP ON LWR SIDE OF FLOORBEAM TOP STRUCTURE BS 344 LBL 12 APPROX. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7SDR UPS03240666Attach Fitting · crackedINSPECTION TYPE: C&SI, RT MLG WING DOOR ACTUATING ROD ATTACH FITTING CRACKED FITTING REPLACED IAW EO B727-3210-2583-G APP. D, E, F & GSDR UPS03240654Web · crackedINSPECTION TYPE: C&SI, NOSE WHEEL WELL LT SIDE AT STA 992 WL 140 TWO SMALL CRACKS ON HORIZONTAL WEB. HORIZONTAL WEB REMOVED & REPLACED IAW SRM 51-20-01 & 51-30-02SDR UPS03240642Radome · damagedINSPECTION TYPE: C&SI, RADOME FAILED MOISTURE CHECK. RADOME REPLACED IAW MM 53-15-00. RESISTANCE CHECK CARRIED OUT ON RADOME IAW MM 53-15-00. CHECK FOUND TO BE SATISFACTORYSDR UPS03240683Tab · delaminatedINSPECTION TYPE: C&SI, LT WING, I/B AILERON TAB HAS 2 ARMS OF DELAMINATION ON UPPER SURFACE. I/B AILERON TAB REMOVED IAW MM 27-10-05. FITTED NEW AILERON TAB IAW MM 27-10-05. I/B AILERON TAB BALANCE CHECKED IAW SRM 51-80-03. ADJ /TEST CARRIED OUT IAW MM 2SDR UPS03240667Angle · corrodedINSPECTION TYPE: C&SI, SURFACE CORROSION ON ANGLE AT LWR END OF BS 950 FITTING LT AT STR. 22 LT IN LT MLG WHEEL WELL. REPAIR CARRIED OUT IAW SMRO EO 2003025009.SDR UPS03240644Attach Fitting · crackedINSPECTION TYPE: C/SI, LT MLG SWIVEL VALVE LINK ARM ATTACH BRACKET CRACKED AT UPPER ATTACH POINT. BRACKET REPLACED IAW SRM 51-20-1SDR UPS03240546Structure · crackedINSPECTION TYPE: C&SI, CRACK AT BELLED HOLE ON VERTICAL WEB ON LT SIDE OF AIRSTAIRS AT STA . 1306 (LOWER HOLE). CRACKS STOP DRILLED IAW SRM 51-10-1. HFEC INSP. CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4 RESULTS - NDF CRACK CONTAINED. REPAIR CARRIED OUSDR UPS03240545Hinge · corrodedINSPECTION TYPE: C&SI, O/B AILERON, LT WING, O/B TAB HINGE HAS EXCESSIVE CORROSION 2ND I/ B IS CRACKED AND THE OTHER TWO ARE PITTED EXTENSIVELY. TAB HINGES REPLACED IAW SRM 51-30-02 FOR O/B AILERON TAB INSTALLATION REF. NRC 664356SDR UPS03240684Frame · corrodedINSPECTION TYPE: C&SI, BODY FAIRING NR 3430, HAS CORRODED FRAME AFT OF GND. COOLING FAN DOOR CUT OUT. FRAME REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06 OUT OF LIMITS IAW SRM 51-10-01. NEW FRAME FABRICATED IAW SRM 51-20- 1 FIG 7. NEW FRASDR CA030312024Bungee Cylinder · frozen(CAN) AFTER DEPARTURE WHEN GEAR SELECTED UP, NOSE GEAR IND SHOWED DOWN AND LOCKED. AIRCRAFT RETURNED TO YHM. MAINT REPLACED NLG POSITION AND LOCK SWITCHES (NOSE). AIRCRAFT DEPARTED AND RETURNED AGAIN. CREW REPORTED GEAR REMAINED EXTENDED. MAINT FOUND NLG LOSDR UPS03240107Skin · crackedINSPECTION TYPE:C+SI 5 MM CRACK FOUND PROPAGATING FROM THE SIXTH FASTENER I/B OF STR.4 R AT BS360 AFT SKIN AFT FASTENER ROW. FASTENERS REMOVED IAW SRM 51-30-02. CRACK TRIMED OUT IAW SRM 51-10-06 REPAIR CARRIED IAW EO.B727-5310-1371+DRG.NO.69-62161.SDR UPS03240121Beam · corrodedINSPECTION TYPE: C&SI, RT HORIZ STAB UPPER T/E BEAM BETWEEN RIB AT STR 66.50 & STR 99.76 IS CORRODED UNDER RUBSTRIP. BEAM REPLACED IAW DRAWINGS 65-20657, 65-20658, 65-20659, 65-20660-65 22402 & 65-22987SDR UPS03240102Seal · crackedINSPECTION TYPE: C&SI, NR 6 & 8 LEADING EDGE SLAT CRACK FOUND AT I/B END UNDER PORK CHOP SEAL. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 5.SDR UPS03240133Skin · crackedINSPECTION TYPE:SP CRACK FOUND ON FUSELAGE ABOVE # 1 ENGINE STATION 1183 STRINGER 4L-8L REMOVED PREVIOUS REPAIR DOUBLER AND DAMAGED AREA I.A.W. SRM.53-30-3 FIG. 26 & 24, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I.A.W. SRM. 53-30-3 FIG. 26 & 24 ATSDR UPS03240094Frame · corrodedINSPECTION TYPE: C&SI, FAIRING 3429 HAS CORRODED FRAME SECTION ABOVE ACCESS PANEL 3420. CUTOUT CORRODED FRAME SECTION, REMOVED IAW SRM 51-30-2. NEW FRAME SECTION FABRICATED IAW SRM 51-20-1 FIG 7 AND SRM 53-50-1 FIG 2. NEW FRAME SECTION INSTALLED IAW SRM 51-SDR UPS03240115Web · chafedINSPECTION TYPE: C&SI, LT STAIRWELL HORIZONTAL WEB IS CHAFED UNDERNEATH LT & RT AIRCON. FLOW CONTROL & SOV'S. REPAIR CARRIED OUT IAW SRM 51-40-02.SDR UPS03240108Carriage · corrodedINSPECTION TYPE: C+SI, NR 3 FLAP CARRIAGE HAS CORROSION AT BASE OF SPINDLE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03 DUE TO CORROSION.SDR UPS03240114Stringer · crackedINSPECTION TYPE:C&SI CRACK IN AIRSTAIR CENTRE STRINGER AT LWR END OF 2ND BAY FROM TOP OF STAIR REPAIR CARRIED OUT AS REQUIRED IAW SRM 53-10-3SDR UPS03240126Support · corrodedINSPECTION TYPE: C+SI, CORROSION ON TOILET SUPPORT BEAM BETWEEN BS 328 AND 344. INSTALLED NEW SUPPORT BEAM AT ABOVE LOCATION IAW SRM 51-30-2.SDR UPS03240120Flange · corrodedINSPECTION TYPE:C&SI R/H W/W BS 930 HORIZ. INTERCOSTAL COMMON TO BS 930 FRAME EVIDENCE OF CORROSION ON HORIZ. AND VERTICAL FLANGE REPAIR CARRIED OUT IAW SMRO EO 2003-003-013 UPS ENGINEERING FILE NO. 727-53-20093SDR UPS03240118Hinge · crackedINSPECTION TYPE: C&SI, SMALL CRACK ON RT WING UPPER T/E AT SPOILER NR 11 OUTER HINGE CUTOUT. REPAIR CARRIED OUT IAW SRM 57-30-4.SDR UPS03240093Floorbeam · corrodedINSPECTION TYPE: C&SI, SURFACE CORROSION ON FLOORBEAM TOP CAP BS 312 LBL 10 & LBL 24.75. CARRIED OUT REPAIR AT ABOVE LOCATION IAW SRM 53-10-8.SDR UPS03240113Channel · crackedINSPECTION TYPE:C&SI BS1263 R/H, VENTRAL STAIR TORQUE BOX HORIZ. BEAM IS CRACKED AT I/B U PPER RADIUS CHANNEL REPLACED IAW DRAWING 65C13874& SRM 51-30-02SDR UPS03240110Stiffener · corrodedINSPECTION TYPE:C&SI CORROSION AT FLOOR LEVEL I/B STIFFENER BS 233 APPROX RBL 16 APPROX U NDERNEATH 1ST OFFICERS SEAT SUPPORTS CORROSION REMOVED AND FOUND OUTSIDE LIMITS OF SRM 51-10-6 & 51-10-1 STIFFENER CHANNEL REPLACED IAW SRM 51-30-2SDR UPS03240125Fitting · corrodedINSPECTION TYPE:C&SI ON #3 SPOILER ACTUATING QUADRANT DISCONNECTION #3 SPOILLER SUPPORT F ITTING FOUND TO BE CORRODED BEYOND THE LIMITS REPLACED FITTING IAW DRAWING 65-21622-22 & MM 20-10-05SDR UPS03240100Bracket · crackedINSPECTION TYPE:C&SI BRACKET CRACKED AT MAIN CARGO DOOR SUPPORT BEAM BS 580 STR. 2 L/H REPAIR CARRIED OUT IAW SMRO EO 2003-003-008 UPS ENGINEERING FILE NO. 727-55-20034SDR UPS03240095Support · corrodedINSPECTION TYPE:C&SI CORROSION ON SEAT TRACK SUPPORT BS 850 - 870 RBL 62.5 SUPPORT REPLACED IAW SRM 51-30-02SDR UPS03240128Flap Track · corrodedINSPECTION TYPE:C+SI NO.3 FLAP TRACK HAS CORROSION ON PAD B, BETWEEN HOLES G AND F AND AL SO ON THE LWR FLANGE AROUND HOLE G. REPAIRED IAW SMRO EO 2003-003-010 AND EO 2003-003-003.SDR UPS03240119Skin · crackedINSPECTION TYPE: C&SI, LOWER RUDDER TAB HAS AN AREA OF DELAM AT LWR AFT CORNER RT SIDE. SKIN CRACK AND LARGE DENT ON LT SIDE 12TH FROM BOTTOM ON T/E AREA LOWER RUDDER TAB REPLACED IAW MM 27-20-11.
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