Boeing 727-27C
Service difficulty reports · 1,078
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 = '72727C' 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 = '72727C' 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 UPS99231078Pressure Web · crackedINSPECTION TYPE:C NOSE WHEEL WELL RIGHT SIDEWALL PRESSURE WEB CRACKED AT BS235.8, WL17 0. (JUST BELOW PRESSURE PANEL) CRACK VERIFIED PER NDT PART 6, 51-00-00 HFEC. STOP DRILLED CRACKS. T RIMMED OUT DAMAGED AREA. INSTALLED REPAIR ON RIGHT PRESSURE WEB BS23 5SDR UPS99231077Pressure Web · crackedINSPECTION TYPE:C NOSE WHEEL WELL LEFT SIDEWALL PRESSURE WEB CRACKED AT BS259.5, WL190 (TWO INCHES BELOW CEILING). CRACK VERIFIED PER NDT PART 6, 51-00-00 HFEC. STOP DRILLED CRACKS ON SIDEWALL PRESSURE WEB. CUT-OUT DAMAGED AREA AT NOSE WHEEL WELL LEFT SIDESDR UPS99231076Pressure Web · crackedINSPECTION TYPE:C NOSE WHELL WELL CEILING PRESSURE WEB CRACKED AT BS277, WL194. CRACKS VERIFIED PER NDT PART 6, 51-00-00, HFEC. STOP DRILLED CRACKS ON CEILING PRESSURE WEB AT STA 277, WL 194. CRACKS END AT STOP DRILL. REMOVED AND REPLACED DAMAGED SECTION OSDR UPS99231075Skin · crackedINSPECTION TYPE:C LEFT WING OUTBOARD FLAP-FOREFLAP LEADING EDGE SKIN CRACKED AT RIVET HEAD (NR 2 FOREFLAP CARRIAGE). PERFORMED HFEC INSP OF CRACK AT L/W O/B FOREFLAP IAW NDT MANUAL PART 6, 51-00-00, FIG 4. VERIFIED CRACK EXTENDS FROM RIVET HOLE TO SKIN EDGE.SDR UPS99231074Blkhd Stiffener · crackedINSPECTION TYPE:C AFT CARGO COMPARTMENT, BS1183 BULKHEAD, VERTICAL STIFFENER, RBL 8 HAS CRACK INDICATION, TOP OF STRINGER, OUTBOARD SIDE OF STIFFENER. HFEC INSPECTED AND VERIFIED CRACK INDICATION AT TOP OF STIFFENER RBL 8, BS 1183, LENGTH 1.25 INCH IAW NDT MASDR UPS99231073Frame · damagedINSPECTION TYPE:C C/W PERMANENT REPAIR TO OVERWING EXIT FRAMES 783.95 RIGHT, 825.95 LEFT, 825.95 RIGHT, AND 848.95 RIGHT. INSTALLED PERMANENT REPAIRS TO OVERWING EXIT FRAMES BS783.95 RIGHT, 825.95 LEFT, 848.95 RIGHT AS PER UPS E0 B727-5310-12010-A.SDR UPS99231072Bracket · corrodedINSPECTION TYPE:C RT WING AFT SPAR AT WS 380.0 THE NR 6 T/E FLAP JACKSCREW OUTBOARD ATTACH BRACKET HAS CORROSION ON LOWER ATTACH POINT. REMOVED AND REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2.SDR UPS99231053Battery Pack · dischargedEMERGENCY EXIT LIGHT OVER FOWARD ENTRY DOOR COMES ON INTERMITTENLY WITH CORRESPONDING OVERHEAD PANEL SWITCH IN ARM POSITION. REMOVED AND REPLACED BATTERY PACK IN UNIT OVER FORWARD ENTRY DOOR. OPS CHECK NORMAL.SDR UPS99230904Battery Pack · dischargedEMERGENCY EXIT LIGHTS ABOVE FWD DOOR COMES ON. BATTERY PACK LOW. RECHARGED EMERGENCY EXIT BATTERY PER MM 33-55-00. OPS CK GOOD.SDR UPS99231049Light · inopINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AT ENTRY DOOR INOP. REMOVED AND REPLACED EXIT LIGHT ASSY IAW 33-50-00.SDR CA991209032Torsion Link · cracked(CAN) LOWER NLG TORSION LINK HAS A CRACK AT CENTER PIVOT POINT LT LUG. TORSION LINK REPLACED.SDR UPS99230572Skin · damagedINSPECTION TYPE:N/A, RIGHT I/B FORE FLAP SKIN PEELED BACK AND CRACKED L/E NEXT TO SPRING DOOR. *S/D* REMOVED NAD REPLACED RIGHT FOREFLAP PER MM 27-51-05. (P/N 65-21 630-92) ON, (P/N 65-21630-174) OFF, (S/N BN119) ON, (S/N 126) OFF.SDR UPS99230253Tab · damagedLEFT OUTBOARD AILERON IE WEDGE OUTBOARD OF TAB HAS CORNER MISSING. REPAIRED PER SRM 57-50-01.SDR 99FDEA00278Switch · sticksAFT CARGO DOOR LIGHT ILLUMINATED AFT T/O, LIGHT EXT ON APPROACH, AT APPROACH SPD. FOUND INNER DOOR SWITCH STUCK. LUBED SWITCH, OPS CK NORMAL.SDR UPS99230086Switch · inoperativeATB - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR SAFETY SWITCH AND LINK ASSY, OPS CHECKS GOOD IAW MM 32-09-21SDR CA990715028Fire Detector · failed(CAN) NR 2 FIRE DETECTION CIRCUIT GROUND LIGHT ON REAR CIRCUIT PANEL ON. REPOSITIONED TWO FIRE LOOP CLAMP GROMMETS ON THE NR 2 ENGINE, TEST SERVICEABLE.SDR CA990630055Clamp · misinstalled(CAN) NR 2 FIRE DETECTION CIRCUIT GROUND LIGHT ON REAR CIRCUIT PANEL. REPOSITIONED TWO FIRE LOOP CLAMP GROMMETS ON THE NR 2 ENGINE CHECK.SDR CA990630053Regulator · malfunctioned(CAN) CAPTAIN'S OXYGEN REGULATOR WILL NOT FUNCTION CORRECTLY IN EMERGENCY POSITION ON. OXYGEN REGULATOR REMOVED AND REPLACED IAW MM.SDR CA990630049Fastener · missing(CAN) WHILE COMPLYING WITH PEMCO SB 727-53-003-001R1 FOR AMC FOR AD 98-23-51 MISSING FASTENERS BETWEEN STA 480 TO 620 WHERE STR 3L WAS REMOVED DUE TO A/C MOD FROM PAX TO CARGO. ALSO SAME FOUND WHERE SECTION OF FRAMES WERE REMOVED DUE TO MOD PER SB. ALL ORIGSDR UPS99229674Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS LEFT ON FROM LAST FLIGHT. RELAMPED AND REPLACED BATTERY, OPS CHECK GOOD.SDR CA990614064Seal · loose(CAN) NOSE GEAR LIGHT COMES ON IN-FLIGHT, NOSE GEAR AREA BANGING ABOVE 320 KNOTS. FOU FOUND DOOR FRONT SEAL LOOSE AND BLOCKING DOOR REPAIRED.SDR UPS99229518Battery Pack · dischargedINSPECTION TYPE:N/A, COCKPIT AND CABIN ENTRY EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN BOTH PACKS. LIGHTS OPS CHECK NORMAL.SDR UPS99229224Fitting · corrodedINSPECTION TYPE:C, LEFT WING OUTBOARD AILERON CENTER OUTBOARD HINGE FITTING CORROED (AILERON SIDE). REPLACED PER SRM 51-30-2.SDR UPS99229210Fitting · corrodedINSPECTION TYPE:C LEFT WING OUTBOARD AILERON CENTER INBOARD HINGE FITTING CORRODED AILERON SIDE. REPLACED HINGE FITTING PER SRM 51-30-2.SDR UPS99229209Rib · crackedINSPECTION TYPE:C, NR 3 SLAT OUTBOARD ACTUATOR RIB IS CRACKED. REMOVED 2 EA RIBS O/B ACTUATOR RIB AND NEXT ONE O/B FOR ACCESS, DRILLED NEW RIB AND INSTALLED, INSTALLED ACCESSED RIB IAW SRM 51-30-02, 51-30-05, 51-10-01.SDR UPS99229213Skin · corrodedINSPECTION TYPE:C WHILE WORKING NRC 923405, FOUND CENTER FUEL CELL UPPER SKIN CORRODED UNDER SEAL RETAINER RBL 50-65. REPAIRED PER ER 99-5206.SDR UPS99229097Support · corrodedINSPECTION TYPE:C CORROSION ON FLOOR SUPPORT BS 680 WL 156 LBL 9. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-10-5.SDR UPS99229215Chord · corrodedINSPECTION TYPE:C, CORROSION ON WING CENTER SECTION AFT LOWER CHORD RBL 42-48 AND AFT UPPER CHORD RBL 38-42. REPLACED UPPER AND LOWER CHORD PER SRM 51-30-2 AND ER 99-5195.SDR UPS99229098Support · corrodedINSPECTION TYPE:C CORROSION ON AFT CARGO PIT FLOOR TRACK SUPPORT ANGLE BS 960, RBL 13.5, WL 155. REMOVED AND REPLACED TRACK SUPPORT PER SRM 51-10-1.SDR UPS99229093Floorbeam · corrodedINSPECTION TYPE:C CORROSION ON FLOORBEAM TOP FLANGE BS 344 LBL 14 - RBL 12 WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-10-8 FIG 9.SDR UPS99229092Support · corrodedINSPECTION TYPE:C CORROSION AFT CARGO FLOOR SUPPORT BS 1046, RBL 10, WL 157. REMOVED AND REPLACED FLOOR SUPPORT SEGMENT PER SRM 53-10-5.SDR UPS99229212Fitting · corrodedINSPECTION TYPE:C, LEFT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-02.SDR UPS99229211Fitting · corrodedINSPECTION TYPE:C, RT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED FITTING PER SRM 51-30-02.SDR UPS99229058Support · corrodedINSPECTION TYPE:C CORRSION ON CHANNEL SUPPORT BS 314-344, RBL 13.5, WL 208 UNDER LAV DOORWAY. REMOVED AND REPLACED CHANNEL SUPPORT PER SRM 51-10-02.SDR UPS99229057Support · corrodedINSPECTION TYPE:C CORROSION ON AFT CARGO BAY FLOOR SUPPORT AT BS 1045, RBL 3, WL 154. REMOVED AND REPLACED SEGMENT OF SUPPORT PER SRM 53-10-5 FIGURE 4.SDR UPS99229096Handle · corrodedINSPECTION TYPE:C CORROSION ON LT AFT OVERWING EXIT DOOR HANDLE AT TORQUE TUBE ATTACHMENT AFTER THE CORROSION REMOVAL, THE HANDLE WENT BEYOND ALLOWABLE LIMITS PER SRM 52-00-2. REPLACED THE HANDLE WITH A NEW ONE AND INSTALLED IT ON THE TORQUE TUBE PER SRM SDR UPS99228971Light · inopINSPECTION TYPE-N/A, EMER EXIT LIGHT (ENTRANCE) ASSY ROBBED FOR A/C 820 (S/N 20896 A 450467). REPLACED ROBBED EMER EXIT LIGHT (P/N ON 10-0067-9) (S/N 22574), OPS CK PER MM 33-50-00. NO DEFECTS NOTED.SDR UPS99229095Support · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON CARGO FLOOR SUPPORT BS 575, RBL 10, WL 156. FABRICATED REPAIR PARTS PER SRM 53-10-5 AND INSTALLED PER SRM 53-10-5.SDR UPS99229094Shear Tie · corrodedINSPECTION TYPE:C CORROSION (C53-133-01-1B) ON FRAME SHIER TIE, BS 700 BETWEEN STR 28R AND STR 28L. SHEER TIE OUT OF LIMITS. FABRICATED NEW TIE AND INSTALLED PER SRM 51 -30-02, SRM 51-10-06, SRM53-10-1, SRM 53-10-4.SDR UPS99229091Floorbeam · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON CARGO FLOOR SUPPORT BS 575, LBL 15 WL 156. FABRICATED REPAIR PARTS PER SRM 53-10-5 AND INSTALLED PER SRM 53-10-5.SDR UPS99229214Link · corrodedINSPECTION TYPE:C CORROSION EMANATING FROM AROUND AFT BUSHING LBL 24 EXPANSION LINK BS 868 WL 205. REMOVED EXPANSION LINK FROM AIRCRAFT, REMOVED CORROSION FROM AROUND BUSHING HOLES AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW EXPANSION LINK AND INSTALLED IASDR UPS99228332Relay · contaminatedINSPECTION TYPE-N/A, DURING DEPARTURE CLIMB PRIOR TO FLAP RETRACTION, THE NR 3 THROTTLE SNAPPED BACK TO IDLE WITH AN AMBER TR WARNING LIGHT ILLUMINATED. NOW ACTUAL AIRFRAME VIBRATION NOTED. THROTTLE WOULD NOT ADVANCE, ENG WAS THEN SHUTDOWN. AIR TURNBACK TO SDR CA981214008Indicator · malfunctioned(CAN) INBOARD FLAPS WOULD NOT EXTEND OR RETRACT. INBOARD POSITION INDICATOR REPLACED.SDR CA981214007Indicator · leaking(CAN) LEFT MACH/AIRSPEED INDICATOR LEAKING, REPLACED.SDR 98FDEA00660Bulb · failedON APPROACH, WHEN GEAR HANDLE PUT DOWN BOTH LIGHTS IN RIGHT MAIN GEAR IND BURN OUT. DID GO-AROUND AND REPLACED BOTH BULBS, WORKED OK. CHECKED MAIN GEAR IND LIGHTS, CHECKS OK.SDR CA981113014Fitting · cracked(CAN) BS 940 FUSELAGE MAIN FRAME FITTING AT FLOOR BEAM ATTACH FLANGES - RIGHT FITTING LOWER FORWARD FLANGE CRACKED FROM EDGE TO FASTENER. LEFT FITTING CRACKED IN WEB AREA. REPAIRED. AD 94-07-08, SB 727-53-0190 REFERS. PART TC: 53,613.SDR CA981113012Bearing · sticking(CAN) RECURRING REPORTS OF AILERONS FAIL TO CENTER, FEEL+CENTERING MECHANISM REPLACED. SUBMITTER STATED FOUND SB 727-27-0154 CAPT AILERON DISCONNECT ASSEMBLY BEARING IMPROPERLY INSTALLED. REPAIRED.SDR UPS98227879Web · crackedINSPECTION TYPE-C, THE AFT STAIRWELL TORQUE BOX INBOARD VERTICAL WEB IS CRACKED JUST UNDER PREVIOUS REPAIR AT BS 1266 WL 192 RBL 21. REMOVED PREVIOUS REPAIR CUT OUT DAMAGED AREA PER SRM 53-10-1. FABRICATED REPAIR DOUBLER PER SRM 51-40-2. INSTALLED DOUBLER PSDR UPS98227589Web · crackedINSPECTION TYPE-C, NLG W/W CEILING HAS VISUAL CRACK INDICATION AT RIVET HOLE STA 288 BL 0. REMOVED AND REPLACED DAMAGED SECTION OF WEB NWW CELING BS 288 TO 270 BL 9 LT TO BL 9 RT AS PER B727 SRM 53-10-2 FIG 2 AND 51-30-2. MATERIAL USED 7075-T6 .040 18 X 18 LSDR 98FDEA00496Switch · malfunctioned98-0197 - NR 2 SLAT STILL IND OUT WHEN FLAP RETRACT TO ZERO POSITION TEST ALL AMBER LEADING EDGE SLATS ILLUM). AIRPLANE DID NOT HOWEVER ROLL LEFT. REQUIRES UNUSUAL CONTROL INPUTS TO KEEP WINGS LEVEL. FOUND NR 2 SLAT ACTUATOR POSITION SWITCH TO BE BAD. REPL
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