Boeing 727-200
Service difficulty reports · 2,835
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 = '727200' 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 = '727200' 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 06FDEA2217Stop Fitting · gougedLEFT AFT SERVICE DOOR FWD LOWER STOP PIN FITTING IS GOUGED. REPAIRED PER FED EX EA 7-5240-100541.SDR 06FDEA2215Structure · corrodedNR 1 K-FLAP CORRODED AT O/B BONDING JUMPER ATTACH POINT. REPAIRED NR 1 K-FLAP PER FED EX EA 7-5710-100544.SDR 06FDEA2216Stiffener · chafedLEFT WING BRACKET LOOSE AND CHAFING ON NR 8 VERTICAL STIFFENER, INBOARD SIDE OF WS 192.01. REPAIRED VERTICAL STIFFENER IAW FED EA 7-5710-100545.SDR 06FDEA2191Stringer Clip · damagedMECHANICAL DAMAGE TO STRINGER CLIP AT BS 480 STRINGER 7RT. REMOVED AND REPLACED STR AND SPLICE AT BS 480 STR 7RT.SDR 06FDEA2039Stringer · corrodedFOUND STRINGER 28 LT TO BE CORRODED AT BS 680-700. REMOVED S28R AND PRODUCTION SPLICES BS 680-700 AND REINSTALLED NEW STRINGER IAW FED EX SRM 51-30-2.SDR 06FDEA2038Stringer · corrodedFOUND STRINGER 28 RT TO BE CORRODED AT BS 680-700. REMOVED S28R BS 680-700 RT & PRODUCTION SPLICES AND REINSTALLED NEW STRINGER PER FED EX SRM 51-30-2.SDR 06FDEA2009Stringer · misrepairedREWORK REQUIRED, REJECTED FOR WRONG REPAIR USED AT BS 1101, STR 29L, REF CARD N01221. REPAIRED STRINGER PER SRM 53-10-3 FIG 1.SDR 06FDEA1827Wedge · chafedUPPER RUDDER, LEFT T/E WEDGE CHAFED APPROX 7.75 INCHES FROM UPPER T/E EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFED APPROX. 7.75" FROM UPPER EDGE UAW FED EX EA 7-5530-100549.SDR 06FDEA1826Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 7.75 INCHES FROM UPPER T/E. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 7.75" FROM UPPER EDGE IAW FEDEX EA 7-5530-100549.SDR 06FDEA1825Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 52 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 52" FROM BOTTOM IAW FED EX EA 7- 5530-100549.SDR 06FDEA1824Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 46.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE APPROX 46.5" FROM BOTTOM IAW FED EX EA 7-5530- 100549.SDR 06FDEA1823Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 43.75 INCH FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 43.75" FROM BOTTOM IAW FEDEX EA 7-5530-100549.SDR 06FDEA1819Wedge · chafedUPPER RUDDER, LEFT T/E WEDGE CHAFED APPROX 2 INCHES FROM BOTTOM EDGE.SDR 06FDEA1817Wedge · chafedUPPER RUDDER LEFT T/E WEDGE CHAFED APPROX 24 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE APPROX 24" FROM BOTTOME IAW FED EX EA 7-5530-100549.SDR 06FDEA1815Wedge · chafedUPPER RUDDER LEFT T/E WEDGE CHAFED APPROX 28.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX 28.5" FROM BOTTOM IAW FEDEX EA 7-5530-100549.SDR 06FDEA1814Wedge · chafedUPPER RUDDER RIGHT T/E WEDGE CHAFED APPROX 28.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX. 28.5 " FROM BOTTOM IAW FED EX EA 7-5530-100549.SDR 06FDEA1813Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 24 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX. 24" FROM BOTTOM IAW FED EX EA 7-5530-100549.SDR 06FDEA1812Wedge · chafedUPPER RUDDER, RT TIE WEDGE CHAFED APPROX 2 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RH T.E. WEDGE CHAFF APPROX 2" FROM BOTTOM EDGE IAW FED EX EA 7-5530-100549.SDR 06FDEA1779Frame · dentedFRAME AT BS 680 BETWEEN STR 24L - 25L HAS DENT. *S/D* REPAIRED FRAME PER SRM 51-40-3.SDR 06FDEA1778Stringer Clip · damagedSTRINGER CLIP BS 1010 STR 7 LT HAS 2 EXTRANEOUS HOLES AND DAMAGE. *S/D* REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA1765Stringer Clip · damagedMECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 8 LEFT. *S/D* FOUND STRINGER CLIP OUT OF LIMITS. REMOVED AND INSTALLED NEW STR CLIP IAW SRM 53-10-1 AND SRM 51-30-2.SDR 06FDEA1764Stringer Clip · damagedMECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 7 LEFT. *S/D* REMOVED DAMAGED STR CLIP, AND INSTALLED NEW CLIP IAW SRM 53-10-1 AND SRM 51-30-2.SDR 06FDEA1762Stringer Clip · crackedSTRINGER CLIP AT BS 540 LT STR 23 CRACKED. *S/D* REMOVED CRACKED STR CLIP. INSTALLED NEW CLIP IAW SRM 53-10-1, 51-30-5 AND SRM 51-30-2.SDR 06FDEA1760Stringer Clip · crackedSTRINGER CLIP AT BS 600 LT STR 23 CRACKED. *S/D* REPLACED STR CLIP PER SRM 53-10-1, 51-30-5.SDR 06FDEA1763Stringer Clip · crackedSTRINGER CLIP AT BS 560 LT STR 23 CRACKED. REMOVED CRACKED STR CLIP AT BS 560 LT STR 23 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. OBTAINED NEW CLIP LOCATED AND DRILLED PER SRM 51-30-5 AND INSTALLED PER SRM 51-30-2.SDR 06FDEA1739Skin · out of limitsN01802 WHILE WORKING N01403, BLENDED EXTERNAL SKIN AT BS 950D PLUS 15 STR26LH REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 14.SDR 06FDEA1740Skin · out of limitsN01803 WHILE WORKING N01403. BLENDED EXTERNAL SKIN AT BS950E PLUS 13 TO BS9503 PLUS 17 BTWN STR27-26 LT REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 1.SDR 06FDEA1741Skin · out of limitsN01804 WHILE WORKING N01403. BLENDED EXTERNAL SKIN BTWN BS979 TO BS983 BELOW AND AT STR 25LT. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 3.SDR 06FDEA1742Stringer Clip · crackedN00602 STRINGER CLIP AT BS 580 LT STR. 22 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-2.SDR 06FDEA1743Stringer Clip · crackedN00605 STRINGER CLIP AT BS 580 LT STR. 23 CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA1744Stringer Clip · crackedN00610 STRINGER CLIP AT BS 580 LT STR. 24 CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA1720Stringer · corrodedCORROSION IN STRINGER CHANNEL STA 1070 - 1110 STR 29R. INSTALLED REPAIR HAT SPLICE SECTIONS BETWEEN 1080-1120 IAW SRM 53-10-3.SDR 06FDEA1723Skin · dentedEXTERIOR FUSELAGE BS 1148 BETWEEN STR 5R AND 6R, SKIN IS DENTED. FOUND DENT TO BE BEYOND LIMITS. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED REF SRM 53-30-3.SDR 06FDEA1706None · noneFOUND REPAIR LOCATED AT STA 410 STR 15 RT, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSSDR 06FDEA1707None · noneFOUND REPAIR LOCATED AT STA 203 STR 28R REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITSDR 06FDEA1708None · noneFOUND REPAIR LOCATED AT STA 1050 STR 29L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 2, REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 SDR 06FDEA1687Skin · chafedFOUND RIGHT HAND LOWER FUSELAGE OUTER SKIN HAVE MULTIPLE CHAFED DAMAGE APPROX BETWEEN STA 1100 TO STA 1175, AREA BETWEEN STA 1100 TO STA 1110 AND STA 1175 FOUND OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR PARTS IAW SRM 53-30-3 FIG 1 AND REINSTALLED ALL RSDR 06FDEA1656Keelbeam · crackedKEEL BEAM CRACKED, RIGHT SIDE BS 872-B2 874, 2 EA FASTENER HOLES, MARKED, 4 INCHES ABOVE BOTTOM SURFACE OF BEAM. REPAIRED KEEL BEAM UPPER CHORD R/H SIDE AT BS 872-874 IAW FEDEX EA 7-5310-99517.SDR 06FDEA1637Rib · gougedN00638, WHILE WORKING CARD NR 73C023-00 (TAIL 43). FOUND VERT FIN TENSION TIE RIB. RT AFT VERT BOLT HOLE HAS GOUGE. REPAIRED BOLT HOLE PER FED EX EA 7-5530-100866.SDR 06FDEA1638Rib · gougedN00712 WHILE WORKING CARD NO. 73C023-00 (TAIL 43), FOUND VERT. FIN TENSION TIE RIB, LT VERT AFT BOLT HOLE HAS A GOUGE. REPAIRED BOLT HOLE IAW EA 7-5530-100866.SDR 06FDEA1626Engine · damagedPDIS 484 72-00 0008454 27APR06 DFW OPEN LOGPAGES: 00674359 RTO AT 110 KTS,SUSPECTED COMPRESSOR STALL ON NR 3 ENG. NO TEMPERATURE OR ENGINE LIMITS EXCEEDED. ENT BY: 094904 RPT BY: 096724 SHGN 27APR06 15:30 DFW INSPECTED TAILPIPE, FOUND TURBINE WISDR 06FDEA1628Floorbeam · cutCUT MARK INTO VERTICAL FLANGE OF FLOORBEAM JUST BELOW UPPER FLANGE BS 1010 RBL 57 WL 207 AFT SIDE. REPAIRED FLOORBEAM PER SR27-53-034 SHEET 5.SDR 06FDEA1627Floorbeam · cutCUT MARK INTO VERTICAL FLANGE OF FLOORBEAM JUST BELOW UPPER FLANGE BS 990 RBL 57 WL 207 AFT SIDE. REPAIRED FLOOR BEAM PER SR27-53-034 REV F.SDR 06FDEA1625Controller · malfunctionedAUTO AND STBY CONTROLLERS WOULD NOT MAINTAIN CABIN PRESSURIZATION. OUTFLOW VALVE SHOWED FULL CLOSED UNTIL DESCENDING THROUGH 4000 FT MSL THEN WENT FULL 31,000 FT CABIN ALTITUDE WAS 12,000 FT AND CLIMBING 600 FPM IN ALL MODES. CLOSING CARGO HEAT OUTFLOW ONLY SDR 06FDEA1609Rmi · malfunctionedFIRST OFFICERS HSI HAS A -HEADING- FLAG APPEARING ON TAXI. CAPTAIN`S RMI, HSI & F/O RMI APPEAR TO INDICATE THE SAME HEADING. *S/D* REMOVED & REPLACED CAPT'S RMI IAW FEDEX M/M 34-21-051-4.SDR 06FDEA1611Skin · damagedFOUND LOWER CARGO COMPARTMENT EXTERIOR SKIN SURFACE IS DAMAGED BETWEEN STA 1050 TO STA 1070, STR 25R. REMOVED DAMAGE PARTS IAW SRM 53-30-3, FABRICATED REPAIR PARTS IAW SRM 53-30-2 FIG 4 AND INSTALLED DOUBLER REPAIR PARTS IAW SRM 51-30-2 AND SRM 53-30-3 FIG 3 SDR 06FDEA1610Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-30-3 FIG 5 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHSDR 06FDEA1607Repair · unknownFOUND SINGLE RIVET REPAIR LOCATED AT STA 184 FWD OF NOSE ACCESS DOOR, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1575Panel · puncturedPANEL 9117 HAS PUNCTURE ON LOWER SURFACE, I/B END. *S/D* REPAIRED PANEL 9117 PER FED EX EA 7-5510-96628.SDR 06FDEA1573Control Rod · stiffTEST FLIGHT NWS EXTREMELY STIFF TURNING RIGHT. ADJUSTED NWS SYSTEM AND REMOVED AND REPLACED RUDDER PEDAL STEERING CONTROL ROD PER FED EX MM 32-51-000-5.
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