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 96FDEA01612Skin · delaminatedNR 0693, LT I/B FORE FLAP HAS TWO LARGE AREAS OF DENTS AND DELAMINATION ON LOWER SURFACE. *S/D* REPAIRED DAMAGED SKIN TO LT I/B FORE FLAP LOWER SURFACE IAW FEDEX SRM 51-40-6.SDR 96FDEA01607Frame · corrodedNR 0100, CORROSION NOSE E-BAY FRAME BS 203.8 LBL 15 WL 170 UPPER AND LOWER SURFACE OF UPPER CHORD. *S/D* REPAIRED NOSE E-BAY FRAME BS 203.8 LBL 15 WL 170 UPPER AND LOWER SURFACE OF UPPER CHORD PER FEDEX SRM 51-40-4.SDR 96FDEA01606Beam · corrosionNR 0713 004. CORROSION (C53-224-01 (2)) ON LONGITUDINAL BEAM AT BS 807 - BS 812 LBL 45 WL 208. REMOVED AND REPLACED LONGITUDINAL BEAM AT BS 740-848, LBL 45 WL 208.SDR 96FDEA01620Floor Beam · corrosionNR 0186 012. CORROSION (C53-113-01(2)) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1070 LBL 41 - RBL 51 WL 200. REPAIRED LOWER CHORD OF FLOORBEAM AT NUTPLATE HOLES BS 1070, LBL 41-RBL 51, WL 200. PER FEDEX SRM 53-10-8.SDR 96FDEA01635Stringer · crackedNR 0152 025. CRACKED STRINGER AT BS 720 B AND 3 STRINGER 15 LT. REMOVED AND REPLACED CRACKED STRINGER AT BS 720B PLUS 3 TO 720C STR 15 LT IAW FEDEX SRM 53-10-3 FIG 1 DETAIL II.SDR 96FDEA01601Clip · crackedNR 0151 003. CRACKED STRINGER CLIP AT BS 400 STRINGER NR 15 LT AND NR 2 RT. REPLACED STRINGER CLIPS AT BS 400 STR 15L AND 2R PER REDEX SRM 53-10-1.SDR 96FDEA01647Bullnose · corrodedNR 0397 030. CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE I/B LINKAGE ATTACH POINT. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE. FUNCTIONAL TESTED. WORK DONE IAW FEDEX M/M 27-81-1.SDR 96FDEA01596Bonding Jumper · corrodedNR0318 - 002, CORROSION (C 57-562-01-02) NR 4 K-FLAP O/B RIB AT PREVIOUS BONDING JUMPER ATTACH POINT. *S/D* FOUND TO BE OUT OF LIMITS. REPAIRED NR 4 K-FLAP O/B RIB AT BONDING JUMPER ATTACH POINT IAW FEDEX SRM 57-50-3.SDR 96FDEA01595Floor Beam · corrosionNR0180 - 001, CORROSION (C53-113-01, -2) ON LOWER CHORD OF FLOORBEAM AT BS 1010 LBL 1 TO LBL 43 WL 200 AT NUTPLATE HOLES. *S/D* B/S 1010 LBL 1 TO LBL 43 WL 200 REPAIRED LOWER CHORD OF FLOORBEAM PER FEDEX SRM 53-10-8 FIG 8.SDR 96FDEA01580Uplock Sensor · malfunctionedDURING LANDING GEAR EXTENSION, RIGHT HAND MAIN LANDING GEAR RED LIGHT ON CENTER PANEL FLICKERED ON AND OFF WHEN GREEN LIGHT WAS ILLUMINATED. THIS CONDITION CONTINUED THROUGH RECYCLING. ACCOMPLISHED RED TABS FOR MAIN LANDING GEAR FAILURE TO EXTEND. LANDING USDR 96FDEA01610Frame · crackedMAIN CARGO STA 804.5 STR 14R BELL FRAME HAS CRACK. INSTALLED DOUBLER PER SRM 51-40-3.SDR CA961022014Psu Line · loose(CAN) ON TAKEOFF ROLL, #2 ENGINE INDICATED UNDER POWER AND HIGH EGT CONDITION. ENGINE INSPECTED FOR PNEUMATIC LEAKS, NONE FOUND. INSPECTED PRBC PSU LINE AND FOUND LOWER FITTING BACKED OFF ALLOWING PSU PRESSURE LEAK WHICH IN TURN ALTERED THE BLEED SCHEDULING RESDR 96FDEA01570Floorbeam · corrodedMAIN CARGO CORROSION ON FLOORBEAM AT STA 1110 FROM 10 TO 24 LBL. REMOVED CORROSION PER SRM 51-10-6. ALL WITHIN TOLERANCE PER SRM 53-10-1 EXCEPT FOR AREA AT LBL 20 CENTER OF F/B WHICH IS OUT OF TOLERANCE. FABRICATED DOUBLER PER AARD 53-10-07-2 PER AARD 53-1SDR 96FDEA01558Floor Beam · corrodedFORWARD CABIN FLOOR BEAM STA 344 HAS CORROSION BOTH TOP AND BOTTOM OF TOP FLANGE AT NUTPLATE HOLES LBL 30 - RBL 15 (MARKED TOP AND BOTTOM). REMOVED CORROSION PER MM 51-10-6. OUT OF LIMITS AT LBL 4, 12, AND 22 PER 53-10-8 FIG 9. INSTALLED SPLICE ANGLES SDR CA960909028Connector · broken(CAN) ENROUTE TOP OF DESCENT #1 ENGINE FIRE WARNING SOUNDED. FIRE DRILL COMPLETED, BOTTLES FIRED, LIGHT ON. BELL AND LIGHT INITIALLED CANCELLED WHEN FLIGHT IGNITION WAS SELECTED. EMERGENCY LANDING. #1 FIRE WIRE HARNES FAULTY.SDR 96FDEA01426Integral Rib · crackedLT 870 INTEGRAL RIB FWD CRACK FROM O/B HOLE TO EDGE. INSTALLED BATHTUB FITTING PER EA NR 7-5310-28832.SDR 96FDEA01402Skin · corrodedCORROSION IN EXTERNAL SKIN STR 28L STA 715. REMOVED CORROSION PER SRM 53-30-3, INSTALLED DOUBLER PER SRM 53-30-3.SDR 96FDEA01403Skin · corrodedCORROSION ON SKIN I/B OF STR 28R STA 715 EXTERNAL. REMOVED CORROSION PER SRM 53-30-3 INSTALLED DOUBLER PER SRM 53-30-3.SDR 96FDEA01371Floor Beam · corrodedNR0054 AND 012, CORROSION (C53-111-01, -3) ON BOTTOM OF FLOOR BEAM BS 1148 RBL 10.SDR 96FDEA01368Stringer · crackedNR 0511 AND 011. CRACK IN STR 23L BETWEEN STR 380 AND STR 400. ****S/D***** COMING.SDR 96FDEA01362Clip · crackedNR 0471 AND 010. STRINGER CLIP IS CRACKED AT BS 680 STR 3L. ***S/D***** COMING.SDR 96FDEA01349Floor Beam · corrosionNR0465 AND 088. CORROSION C53-224-04 ON FLOOR BEAM OUT OF LIMITS BS 1050 RBL 35 WL 208.1. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES (2 EA), AND REPLACED FILLER ON FLOOR BEAM AT BS 1050 RBL 35 WL 208.1 AND TREATED IAW FEDEX SRM 53-1SDR 96FDEA01348Frame · dentedNR0042 AND 007. DENTS IN FRAME BS 660 STR 23-25L. DENT IN FRAME AT BS 660 BETWEEN STR 24-25L FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. DENT IN FRAME AT BS 660 BETWEEN 23-24L FOUND OUT OF LIMITS (CRACKED). REMOVED DAMAGED AREA, FABRICATED AND INSTSDR 96FDEA01347Frame · dentedNR0469 AND 006. DENTS IN FRAME AT BS 580 BETWEEN STR 16-17R. REPAIRED DAMAGED FRAME AT BS 580 BETWEEN STR 16-17R PER FEDEX SRM 51-40-3.SDR 96FDEA01342Indicator · malfunctionedDURING TAKEOFF RETRACTING FLAPS FROM 15 DEGREES TO 5 DEGREES, OUTBOARD FLAPS LEFT AND RIGHT NEEDLES SPLIT BY 2 NEEDLE WIDTHS AND OUTBOARD FLAP INDICATOR STOPPED MOVING. COMPLIED WITH ASYMMETRICAL FLAP CHECKLIST. REPLACED OUTBOARD FLAP POSITION INDICATOR. CHSDR 96FDEA01344Shear Web · corrodedNR 0467 AND 005. CORROSION C53-224-04 ON BOTTOM SIDE OF WEB BS 1170-1176 RBL - LBL 2 WL 207. REMOVED WEB BS 1170-1176 RBL - LBL 2 WL 207. FABRICATED AND INSTALLED NEW WEB. REMOVED SEAT TRACK BS 1130 - 1183 BL ZERO WL 207. FABRICATED AND INSTALLED SDR 96FDEA01340Frame · dentsNR0470 & 004 DENT IN FRAME AT BS00 BETWEEN STR 15-16R. ****S/D***** REPAIRED DAMAGED FRAME AT BS 500 STR 15-16R AS PER FEDEX SRM 51-40-3.SDR 96FDEA01333Floor Beam · corrosionNR0466 & 003 CORROSION C53-224-04 ON FLOOR BEAM AROUND CLIP NOT HOLE BS 1110 LBL 16 WL 207.9 *****S/D**** REMOVED DAMAGED AREA & FABRICATED REPAIR ANGLES (2 EA) & REPAIR FILLER, INSTALLED & TREATED ON FLOOR BEAM AT BS 1110 LBL 16 WL 207.9 IAW FEDSDR 96FDEA01332Frame Splice · dentedNR0041 & 002 DENT IN FRAME SPLICE BS 520 STR 25L. ****S/D***** REMOVED FRAME CAP FROM BS 520 STR 25L FABRICATED & INSTALLED FRAME CAP IAW FEDEX SRM 51-20-1 ALODINED & PRIMED.SDR 96FDEA01327Stringer · corrodedNR0328 AND 001, CORROSION (C53-111-01, -2) ON STR 27L BS 720A PLUS 10 WL 150 LBL 15. *S/D* REMOVED DAMAGED SECTION FROM 720A PLUS 7 TO 720A PLUS 10. REPAIRED STR SECTION PER FEDEX SRM 53-10-1, 53-10-3 FIG 1.SDR 96FDEA01350Floor Beam · corrodedNR0265 AND 009, CORROSION ON BOTTOM OF FLOOR BEAM BS 1070 LBL 55 TO RBL 65. *S/D* REPAIRED FLOOR BEAM AT 1070 LBL 47 TO RBL 65 IAW FEDEX SRM 53-10-8.SDR 96FDEA01306Oil Bypass Sw · malfunctionedNR 2 ENG SHUTDOWN DUE TO NR 2 OIL FILTER BYPASS LIGHT ON IN FLT AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED MAIN OIL SCREEN. FOUND SMALL PIECES OF CARBON. RAN NR 2 ENG TO T/O POWER FOR 5 MINUTES. REMOVED AND REPLACED LOW OIL SCREEN, FOUND IT CLEANED. RSDR 96FDEA01288Oil Bypass Sw · failedNR 1 OIL BYPASS LIGHT ON IN FLT, OIL PRESS 50, TEMP 90, 3.5 GAL, ALL OK. IT STAYED ON AT IDLE PWR, SHUTDOWN NR 1. A/C RELEASED FOR SERVICE PER MEL 79-2 CAT B EXP 29JUL96. *S/D* REMOVED AND REPLACED NR 1 OIL BYPASS SWITCH. RAN AND OPS CHECK GOOD.SDR 96FDEA01213Switch · failedNR 2 OIL FILTER BYPASS LIGHT ON AFTER TAKEOFF. SHUT DOWN AND RETURNED OIL PRESSURE 45, TEMPERATURE 90, QUANTITY 3.8. AIRCRAFT RELEASED FOR SERVICE PER MINIMUM EQUIPMENT LIST 79-4 CATEGORY B EXPIRATION 12 JUL 96. REF NR 2 OIL FILTER BY PASS INOPERATIVE, CHECSDR 96FDEAO1208Floor Beam · corrodedUPPER LOBE BS 870, RBL 49 TO 51 CORROSION ON TOP FLANGE OF FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-6, THICKNESS READINGS ORIG 0.225, READING AFTER CORROSION REMOVAL 0.019. TREATED, PRIMED AND REWORKED AREA.SDR 96FDEA01177Floor Beam · corrodedFLOOR BEAM UPPER CHORD UPPER SURFACE CORRODED AT STA 344 BL ZERO - LBL 60. REMOVED CORROSION ON UPPER CHORD SURFACE - BEYOND LIMITS PER SRM 51-10-6. REMOVED AND REPLACED TOP TEE ANGLE PER SRM 51-10-1. FLOOR BEAM REPAIRED USING FEDEX END DRAWING SR 27-53-SDR 96FDEA01176Floor Beam · corrodedFLOOR BEAM UPPER CHORD UPPER SURFACE CORRODED STA 870, LB 25 - 45, WL 208. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER 53-10-07-02.SDR 96FDEA01175Stringer · crackedUPPER LOBE, BL 9, 720C, STR 15L CRACKED. REMOVED DAMAGE AND INSTALLED STR SPLICE PER SRM 53-10-3.SDR 96FDEA01161Vor Receiver · malfunctionedIN STABILIZED APPROACH, AUTO PILOT VERY UNSTABLE IN PITCH AXIS A SERVO. AUTO PILOT PTICHES UP AND DOWN WITH ASSOCIATED TRIM RUNS TO TRY AND CAPTURE GLIDE SLOPE. A/C RELEASED FOR SERVICE PER MEL 22-1G CATEGORY C EXP 6-30-96 AUTO PILOT GLIDE SLOPE FUNCTIONS ISDR 96FDEA01158Connector · dirtySCL: ENG NR 2 OIL FILTER BYPASS LIGHT CAME ON AT FLT LEVEL 310, 1 HOUR INTO SECOND LEG. ENGINE SHUTDOWN PER PROCEDURES. NORMAL OIL QUANTITY AND PRESSURE. REMOVED CANNON PLUG FROM LOW OIL PRESSURE SWITCH AND OIL FILTER BYPASS SWITCH AND CLEANED WITH CONTACTSDR 96FDEA01178Support · corrodedSEAT TRACK SUPPORT UPPER CHORD UPPER SURFACE CORRODED STA 758-848, LBL 45. REMOVED AND REPLACED SEAT TRACK SUPPORT PER SRM 51-10-01, STA 758 - 848.SDR AALA960826Light · defectiveDFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY OVERHEAD LIGHT AT ROW 25 INOPERATIVE. REPLACED EMERGENCY OVERHEAD LIGHT ASSEMBLY AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 96FDEA01013Map Light Conn · burnedIMMEDIATELY AFTER TURNING THE NR 1 ON, DURING THE START OF DESCENT A BURNING SMELL WAS NOTICEABLE IN THE COCKPIT. REPEAT WRITE UP, REF 522004. RAN NR 1 PACK, FOUND NO TRACE OF BURNING ODOR. OPENED NR 1 ENG, CHECKED DUCTING, FOUND OK. RAN ENGINE, STILL NO BSDR 96FDEA01012Bleed Syst · odorON DESCENT WHEN NR 1 BLEED SELECTED STRONG BURNING ODOR UNTIL BLEED TURNED OFF. RAN ENGINE AND CHECKED OUT NR 1 BLEED SYS, NO STRONG BURNING ODORS WERE DETECTED. A/C OK FOR SERVICE.SDR 96FDEA01002Qty Xmitter · broken wireLOSS OF 'A' QTY DECREASED FROM 5 GAL TO 1.2 GAL, LEAK STOPPED. PRESSURE NORMAL ENTIRE FLIGHT. REPAIRED WIRE AT A-SYSTEM QTY XMTR, VERIFIED QTY AT SYSTEM 'A' TO PROPER LEVEL. NO LEAKS FOUND OR NOTED.SDR 96FDEA00949Retract Mech · malfunctionedAFTER T/O, NR 4 L/E FLAP WOULD SHOW INTRANSIT, AMBER LIGHT ON SECOND OFFICER'S PANEL. COMPLIED WITH L/E DEVICE MALFUNCTION DURING FLAP RETRACTION A. NR 4 L/E FLAP W/N RETRACT, RETURNED TO MIA. REMOVED JUMPER FROM NR 4 L/E FLAP SWITCH AND RECONNECTED SWITCH.SDR 96FDEA00937Pos Ind Switch · malfunctionL/E DEVICE MALFUNCTION ON FLAP RETRACTION. WHEN FLAPS MOVED TO 2 DEGREE YELLOW L/E FLAP LIGHT IS ON AND 2, 3, 6, 7 AND 4 POSITION TEST LIGHTS ARE GREEN. REPLACED NR 4 FLAP POSITION INDICATING SWITCH IAW MM 27-82-11, OPS CK GOOD.SDR 96FEDA00914Stringer · crackedSTA 640 STR 3R CRACKED IN RADIUS. REPAIRED STR PER SRM 53-10-3 FIG 3.SDR 96FDEA00913Stringer · corrodedCORROSION INSIDE UPPER LOBE AT STR 14R FROM STA 480 TO 720E AT SKIN LAP. REMOVED CORROSION OUT OF LIMITS, INSTALLED DOUBLER PER SRM 53-30-3 FIG 5.SDR 96FDEA0448Seat Track · corrodedNR 0375, 014C CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 LBL 25 WL 208. *S/D* SEAT TRACK CORRODED OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 760 TO 848 LBL 25 WL 208.
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