Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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 = '727233' 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 07FDEA00043Stringer Clip · damagedSTRINGER CLIP HAD UPPER RADIUS GROUND/DAMAGED AT BS 440 STR 2R. REMOVED AND REPLACED STRINGER CLIP AT STA 440 STR 2R, REF SRM51-30-02 PG 2.SDR 07FDEA00038Stringer Clip · damagedSTRINGER CLIP HAS BEEN GROUND/DAMAGED IN RADIUS CUT OUT AT BS 660 STR 4L WO NR 35039 SNRM NR N00734. REMOVED AND REPLACED STR CLIP AT BS 660 STR 4L CLASSIFIED AS A MAJOR REPAIR REF SRM 51-30-2 PG 1.SDR 07FDEA00037Stringer Clip · damagedSTRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT AT BS 660 STR 6L WO NR 35039 SNRM NR N00736. REMOVED AND REPLACED WITH NEW STRINGER CLIP AT STA BS 660 STR 4L CLASSIFIED AS A MAJOR REPAIR REF SRM 51-30-3 PG 1.SDR 07FDEA00036Stringer Clip · damagedSTRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT BS 660 STR 9L WO NR 35039 SNRM NR N00739. REMOVED AND REPLACED WITH NEW SRT CLIP AT BS 660 STR 9L. THIS CLASSIFIED AS A MAJOR REPAIR REF SRM 51-30-2 PG 1.SDR 07FDEA00040Stringer Clip · damagedSTRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT AT BS 660 STR 1R. REMOVED AND REPLACED STRINGER CLIP AT BS 660 STR1R ERF SRM 51-30-2 PG 1.SDR 07FDEA00039Stringer Clip · crackedSTRINGER CLIP IS CRACKED AT RADIUS CUT OUT AT BS 660 STR 3R. REMOVED AND REPLACED STR CLIP WITH NEW AT BS 660 STR 3R REF 51-30-2 PG 1.SDR 07FDEA00024Stringer Clip · damagedSTRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT BS 440 STRINGER 6L WO NR 35039 SNRM NR N00724. REMOVED DAMAGED STRINGER CLIP DRILLED HOLES AND INSTALLED NEW STRINGER CLIP REF SRM 51-30-02 CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00025Stringer Clip · damagedSTRINGER CLIP HAS GROUND AT RADIUS CUT OUT BS440 STRINGER L7 REMOVED DAMAGED STRINGER CLIP, DRILLED HOLES IN NEW CLIP AND INSTALLED REF SRM 51-30-02 PG 2-5.SDR 07FDEA00023Sill · crackedFOUND MAIN DECK CARGO DOOR UPPER SILL UPPER FLANGE CRACKED AT RIVET BUCKTAILS AT STATIONS 575.5, 584, 590 & 596. REMOVED CRACKED SILL REF SRM 51-30-2. FABRICATED SILL REF FED EX DWG 53FX1467. DRILLED UP AND INSTALLED INSTALLED SILL AND STRUCTURE REF SRM SDR 06FDEA04327Relay · malfunctionedCRUISE FL 340 CAPTS FIRE WARNING CUBE SHOWED A SUBTLE GLOW A COUPLE OF TIMES (F/O'S DID NOT) NO OTHER FIRE INDICATIONS. LIGHT DID NOT GLOW AGAIN THEN S/O NOTICED A STEADY LIGHT IN THE APU HANDLE, (APU OFF) PULLED HANDLE, LIGHT REMAINED. DISCHARGED AGENT, LIGSDR 06FDEA04329Doubler · corrodedFWD LOWER FUSELAGE STA 720A - 720B, STR 26R - STR 27R EXFOLIATION CORROSION ON DOUBLER REMOVED AND REPLACED DOUBLER REF SRM 51-30-02 PG 2 AND DRAWING NR 65-80692 SH 3/2.SDR 06FDEA04254Control Cable · out of rigTHE L/GEAR EXTENDED IN FLT WITH GEAR HANDLE IN THE OFF POS. THE EXTENSION WAS UNCOMMANDED WHILE THE GEAR WERE UP AND LOCKED AND THE HANDLE IN THE OFF POS. THE A/C WAS CLIMBING THRU 3K FT AT 180 KIAS AND FLAPS 15. THE MAIN GEAR SHOWED DWN AND LOCKED BUT THE SDR 06FDEA04242Retaining Nut · missingON CLIMB-OUT WHEN FLAP HANDLE WAS RAISED FROM 5 DEG TO 2 DEG, OBSERVED THE INBD FLAP GAUGE STOPPED AT 3/4 DEG. INBD FLAPS INDICATOR REMAINED AT 3-4 DEG FOR LNDG. QRH ACCOMPLISHED. INSP ALL FLAPS AND DISCOVERED LT INBD FLAP INBD JACKSCREW FAIRING END RETAISDR 06FDEA04203A/C Pack · inoperativeON CLIMB-OUT "AUTOFAIL" ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE IN "AUTOSTANDBY" OR "MANUAL" MODES. CONTINUED FLIGHT AT 10,000 WITH CABIN ALTITUDE OF 80 00. OUTFLOW VALVE SEEMED TO WORK NORMAL. REF 727 WDM 21-61-01 CHECKED FOR PWR AND GROUNDS AT CONNSDR 06FDEA04184Frame · crackedMAIN CARGO DOOR LOWER SILL AFT STUB FRAME AT STATION 540 IS CRACKED ALONG INBD RADIUS. FABRICATED AND INSTALLED NEW STUB FRAME PER FEDEX DWG 53FX1349 REV F AND SRM 51-30-02 PG 13.SDR 06FDEA04183Frame · crackedMAIN CARGO DOOR LOWER SILL AFT STUB FRAME AT STATION 560 IS CRACKED ALONG INBD RADIUS. FABRICATED AND INSTALLED NEW STUB FRAME PER FEDEX DWG 53FX1349 REV F AND SRM 51-30-02 PG 13.SDR 06FDEA04127Flap System · malfunctionedDURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD TRAILING EDGE FLAPS WENT ASYMETRIC AND LOCKED OUT AT 2 DEGREES. FOLLOWED QRH PROCEDURES. LANDING UNEVENTFUL. REMOVED AND REPLACED INDICATOR PER M/M 27-52-000-0 SYSTEM OPS CHECKS OK AT THIS TIME. PREMATURE REMOVSDR 06FDEA04095Hydraulic Line · brokenTOTAL LOSS OF HYD SYS A IN FLT FOUND A SYS HYD RETURN LINE BROKEN JUST O/B OF NR 3 SPOILER, ADDED MPN 65-17840-492, CPN 0029943 QTY 1 TUBE AY MSN 1018327 MANUFACTURE HYD LINE O/B OF NR 3 SPOILER REF 727-200 MM 20-10-005-8. INSTALLED SAME. NEEDS LEAK CK. INSDR 06FDEA03917Friction Brake · out of adjustON T/O AND CLIMB NR 2 THROTTLE CONSTANTLY CREEPS FORWARD 3-4% N1. THROTTLE NEEDS TO BE CONSTANTLY PULLED BACK NOT TO OVERSPEED ENGINE. ADJUSTED NR 2 ENG FRICTION BRAKE PER 727-200 M/M 76-11-001-8. OPS CHECKED NORMAL.SDR 06FDEA03746Skin · crackedMAIN ENTRY DOOR EXT SKIN AFT UPPER CORNER HAS 2 CRACKS. REPAIRED MAIN ENTRY DOOR AFT UPPER DOOR IAW SRM 52-00-. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063 C BATCH 986936, FILLER FROM 2024 T-3 .050C BATCH 1136567 TREATED AND PRIMED IAW SRM 51-10-2. INSTASDR 06FDEA03677Switch · faultyON CLIMB-OUT, AMBER LE FLAP LIGHT AT FLAPS 2. POSITION TEST SHOWED GREEN ON SOME SLATS AND FLAPS BUT NO AMBER. COMPLIED WITH QRH. ON POST FLIGHT, VERIFIED WITH CREW THAT THE NR 1 O/B SLAT WAS STAYING SOLID GREEN ON POSTION TEST. REMOVED AND REPLACED NR 1SDR 06FDEA03643Frame · tool damageWHILE WORKING N01192 FOUND DRILL START IN FRAME AT BS 520 STR 26R. REPAIRED FRAME PER SRM 53-10-1, SRM 51-40-3.SDR 06FDEA03632Frame · crackedFRAME AT BS 1352 INNER STRUCTURE CRACKED AT 8:00 POSITION FOUND UPON REMOVAL OF OUTER CHORD. REPAIRED INNER STRUCTURE ON FRAME STA 1352 IAW SRM 51-40-3.SDR 06FDEA03629Attach Fitting · crackedLT WING NR 4 FLAP TRACK FALSE SPAR ATTACH FITTING CRACKED AND SEVERAL FASTENERS LOOSE. FABED NEW WEB SECTION, DOUBLER, ANGLE, AND SPLICES; AND INSTALLED IAW DWG SR27-57-038 REV C AND EA 7-5750-102761, (WING SPOILER SUPPORT BEAM-REPAIR) EA ATTACHED TO SNRM N008SDR 06FDEA03627Spar · failedRT WING FALSE SPAR FASTENERS LOOSE AT NR 5 FLAP TRACK ATTACH AREA REMOVED DAMAGED ANGLE AND WEB, FABRICATED NEW WEB SECTION, DOUBLER AND ANGLE SECTION WITH SPLICE ANGLES IAW DWG. SR 27-57-038 REV C. AND EA 7-5750-102761. ALL PARTS ALODINED AND PRIMERED IAW SRMSDR 06FDEA03619Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE CORRODED BODY STATION 680 BUTT LINE 0 RBL 55. REMOVED CORRODED FLOORBEAM TEE STA 680 IAW B727 SRM 53-10-8.SDR 06FDEA03609Valve · leakingNR 1 ENG FAILED DURING FLIGHT. 1ST INDICATION WAS EXCESSIVE NR 1 FUEL FLOW AND 2 KNOB DIFF BETWEEN NR 1 THRUST LEVER AND NR 2/3. JUST PRIOR TO FAILURE, NR 1 EPR 1.6 (2/3 EPRS 1.8). NR 1 N1 80 NR 2/3 N1S 85) N2 86 (NR 2/3 N2S 88/90) NR 1 FF 4000 (2/3 3400). SDR 06FDEA03602Keelbeam · crackedLT KEELBEAM CRACKED AT BS 872 INSIDE KEELBEAM BOX. REMOVED DAMAGE LT KEELBEAM AT BS 872 AND REPAIRED IAW FED EX EA 7-5310-100593.SDR 06FDEA03601Pressure Panel · corrodedLT WHEEL WELL, CEILING IS CORRODED BS 901, LBL 61. REMOVED CORROSION BS 901, LBL 61 AND REPAIRED IAW FED EX EA 7-5310-100592.SDR 06FDEA03595Rib · corrodedFOUND LT NR 1 ELEVATOR THRUST HINGE RIB IB AND OB LUGS IB AND OB FACES CORRODED/WORN. REPARIED PER FED EX EA 7-5510-100595.SDR 06FDEA03587Switch · malfunctionedNR 5 LEADING EDGE FLAP WOULD NOT RETRACT. FLAP RETRACTED NORMALLY. PROBLEM IS WITH INDICATION. REPLACED NR 5 L/E FLAP SWITCH PER MM 27-82-001-4. OPS CHECKS NORMAL OK FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 40174.SDR 06FDEA03571Torque Link · scratchedON LANDING ROLLOUT BELOW 80 KNOTS, FELT A VIOLENT SHUDDERING FROM THE NOSE WHEEL AREA. AFTER BLOCKING A/C AND INSP'ING NOSE GEAR FOUND DAMAGE AS FOLLOWS: GROUND SHIFT ROD BROKEN AT LWR TORQUE LINK,RT FWD GEAR DOOR HAS A HOLE IN IT,LWR TORQUE LINK SCRATCHSDR 06FDEA03577Throttle · unknownAFTER LEVEL OFF AT FL 320, F/O NOTED THE NR 2 THROTTLE MOVED ITSELF TO FIREWALL POWER WHILE THROTTLES 1 AND 3 REMAINED AT CLIMB POWER. IMMEDIATELY RETARDED THE THROTTLE BACK TO MATCH 1 AND 3. EPR ON NR 2 WAS 2.57 AND TEMP EXCEEDED 650 DEG. OVERBOOST APPROX SDR 06FDEA03484Floorbeam · damagedFOUND FLOORBEAM STA 1130 RBL 50 WL 208 HAS A DOUBLE HOLE ON AFT FLANGE. REPAIRED FLOORBEAM AT BS 1130 RBL 50 WL 208 IAW SRM 53-10-8M THIS IS A MAJOR REPAIR.SDR 06FDEA03483Angle · crackedFOUND VERTICAL STAB, CRACK IN ANGLE, ATTACHED TO UNDER SIDE OF STR 11R, 4" AFT OF TOP OF 1342 BULKHEAD. REMOVED CRACKED ANGLE AT FIN STA. 13.746 UNDER STR 11R, 4" AFT OF BS 1342 BULKHEAD, FABRICATED REPLACEMENT ANGLE FROM .040" 7075-T6 LOT #694306 PER DWG 6SDR 06FDEA03482Bulkhead · crackedFOUND VERTICAL STAB, FRAME FLANGE IS CRACKED IN HALF AT STR 11R, 4" AFT OF TOP OF 1342 BULKHEAD. REMOVED, FABRICATED AND INSTALLED FLANGE PER SRM 51-30-2SDR 06FDEA03481Bulkhead · crackedFOUND VERTICAL STAB, CRACK IN WEB 3" BELOW STR 11L, 8" AFT OF TOP OF 1342 BULKHEAD. BULKHEAD REMOVED, FABRICATED AND INSTALLED WEB PER SRM 51-30-02SDR 06FDEA03480Skin · dentedFOUND EXTERIOR SKIN ID DENTED AT STA 1380, ABOVE NR 2 ENGINE, LT SIDE. REMOVED DAMAGE AT BS 1380 ABOVE NR 2 ENGINE LT SIDE AND REPAIRED IAW SRM 51-30-3, 51- 30-2SDR 06FDEA03467Frame · misdrilledFOUND INTERIOR CABIN, BS 720E FRAME HAS MISDRILLED HOLE 1" ABOVE STR 7L. REMOVED DAMAGE IN FRAME BS 720E STR 7L AND REPAIRED IAW SRM 53-10-4.SDR 06FDEA03466Skin · chafedINTERIOR CABIN, MCD CUTOUT RESTRAINT WEB SKIN IS CHAFED AT BS 631, WL 235. REPAIRED MCD CUTOUT RESTRAINT WEB IAW SRM 51-40-2 FIG 1 AND REPAIRED IAW SRM 51-40-2 FIG 1.SDR 06FDEA03465Stringer · gougedFOUND STRINGER 16 LT BS 388 TO BE GOUGED. REPAIRED STRINGER 16 LT IAW SRM 53-10-3 FIGURE 2 DETAIL II.SDR 06FDEA03464Shear Tie · gougedFOUND FWD CARGO BAY GOUGE IN WEB OF FRAME COMMON TO SHEAR TIE STA 600 BETWEEN STR 27L - 28L. REPAIRED DAMAGED SHEAR TIE ON FRAME BS 600 BETWEEN STR 27L-28L IAW SRM 53-10-4 FIG 13.SDR 06FDEA03468Web · corrodedAFT CARGO COMPT BILGE AREA SUPPORT WEB HAS CORROSION BETWEEN STA 1070-1090 RBL 3. FABRICATED NEW WEB ON TRVLR T6/629725. LOCATED AND DRILLED NEW WEB IAW SRM 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW WEB IAW 51-30-2 SRM.SDR 06FDEA03457Module · crackedSHORTLY AFTER LEVELOFF AT FL310, SYS A HYDRAULIC PUMP LIGHTS FLICKERED AND QUANTITY RAPIDLY DROPPED TO (ZERO). COMPLIED W/QRH AND LANDED IN MEM. FOUND HYD PRESS. LINE FROM NR 1 ENG TO "A" SYS MODULE CRACKED. INSTALLED NEW HYDRAULIC LINE AT "A" SYSTEM MODSDR 06FDEA03463Switch · stickingDURING GEAR EXTENSION NOSE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER EXTENSION WITH DOOR LIGHT ON S/O PANEL. LIGHT WENT OUT AFTER 2 MINUTES. INSPECTED SWITCH ASSY ON NOSE WHEEL GEAR DOOR SWITCH. FOUND PLUNGERS STICKING. CLEANED AND LUBED SWITCH. OPS CHECSDR 06FDEA03460Frame · dentedFWD CARGO BAY DENT IN FRAME INNER FLANGE STA 660 BETWEEN STR 23R - 24R. REMOVED DAMAGE ON FRAME STA 660 BETWEEN STR 23R - 24R AND REPAIRED IAW SRM 51-40-3 AND 53-10-1.SDR 06FDEA03459Frame · dentedFWD CARGO BAY DENTS IN FRAME STA 600 BETWEEN STR 22L-25L. REMOVED DAMAGE ON FRAME BS 600 BETWEEN STR 22L - 25L AND REPAIRED IAW SRM 51-40-3.SDR 06FDEA03458Skin · dentedEXTERIOR SKIN IS DENTED ON AIRSTAIR, AFT LT EDGE. REMOVED DAMAGE ON AIRSTAIR AND REPAIRED IAW SRM 51-40-2.SDR 06FDEA03453Skin · chafedRT AFT EMERGENCY EXIT HAS CHAFE ON LOWER SKIN. REMOVED DAMAGE ON RT AFT EMERGENCY EXIT AND REPAIRED IAW SRM 52-00-3.SDR 06FDEA03452Bulkhead · crackedFWD SIDE 178 BULKHEAD HAS DRILL START ON STRAP UNDER UPPER RT RADAR MOUNT BRACKET. REPAIRED DAMAGE ON 178 BULKHEAD STRAP IAW SRM 51-40-3.
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