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 FDEA201101240338Torque Box · crackedAFT AIRSTAIR AREA RT TORQUE BOX WEB CRACKED AT BS 1327. TRIMMED OUT DAMAGED AREA TO 1 RADIUS IAW SRM 51-40-2 ON AFT AIRSTAIR AREA RT TORQUE BOX WEB. FABRICATED DOUBLER FROM 7075T6 .032 DIM: 3.7500" X 2.7500" IAW SRM 51-40-2 AND INSTALLED DOUBLER IAW SRM 51-3SDR FDEA201101200309Skin · damagedUPON REMOVING MCD SILL, FOUND SKIN DAMAGE FROM RIVET HOLE, STA 540, STR 2L. CUTOUT DAMAGED SKIN AREA, FABRICATED DOUBLER, TRIPLER, & FILLERS, AND INSTALLED REPAIR AT BS 540 S2L IAW EA 7-5310-143936.SDR FDEA201101200315Door Frame · corrodedC-3 DOOR CUTOUT, FRAME IS CORRODED AT FASTENERS ON FWD SIDE BS 1183 BTWN S27-26R. REMOVED FASTENERS & FOUND TO BE OUT OF LIMITS & CORROSION, IAW SRM 51-30-2 & 53-10-1. REMOVED DAMAGE AT SHEAR TIE IAW SRM 53-10-1 REV 103, FABRICATED NEW DOUBLER, NEW FILLER & SDR FDEA201101190286Seat Track · corrodedCORROSION FLOATING SEAT TRACK MAIN CABIN STA 870 TO STA 850, LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK IAW SRM 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 & SRM 53-10-2 FIG 7A.SDR FDEA201101190289Seat Track · corrodedCORROSION FLANGE SEAT TRACK STA 870 - STA 850, RBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK IAW SRM 51-30-5 & DWG 53FX1497 INSTALLED SEAT TRACK IAW SRM 51-30-2.SDR FDEA201101190288Seat Track · corrodedCORROSION FLANGE SEAT TRACK STA 870 -STA 850, BL 0. REMOVED FLOATING SEAT TRACK AT STA 870-850, BL 0 IAW SRM 51-30-2 AND FABRICATED NEW FLOATING SEAT TRACK FROM BAC 1520-14317178, T6511 IAW SRM 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 & SRM 53-10-2,SDR FDEA201101180222Controller · failedDURING CRUISE FLIGHT THE ALTITUDE WARNING HORN SOUNDED. THE CABIN ALTITUDE WAS APPROACHING 11,000 FT & RISING. RAN THE QRH & CHECKED THE PANEL WHICH OFFERED NO RELIEF, THEN IAW THE QRH. WE DESCENDED TO 10,000'. SELECTED THE STANDBY MODE. STILL NO RELIEF. SDR FDEA201101180270Seat Track · corrodedCORROSION SEAT TRACK STA 1176 - STA 1130, BL 0. REMOVED SEAT TRACK STA 1176 TO STA 1130, BL 0 IAW SRM 51-30-2 & SRM 51-10-6. FABRICATED NEW SEAT TRACK DWG 53FX976, REV B 7675T651 0.5X4 DIM: 45" X 3.5". INSTALLED SEAT TRACK IAW SRM 51-30-2.SDR FDEA201101170215Door Frame · crackedFWD ENTRY DOOR, AFT FRAME IS CRACKED AT LOWER CORNER, CRACK GOES UNDER STOP FITTING. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EA7-5210-123580.SDR PCSA2011011801Fire Detector · unsecureNR 1 STRUT OVERHEAT LIGHT ILLUMINATES WITH NR 1 ENGINE BLEED AIR VALVE CLOSED. MECH FOUND FIRE DETECTOR UNIT UN-SECURED. RE-RACKED AND SECURED FIRE DETECTOR UNIT, OPS CHECK GOOD.SDR FDEA201101160186Sill · damagedUPPER SILL BS 541 ON UPPER FLANGE HAS FASTENERS WITH INSUFFICIENT ED. ACCOMPLISHED MCD UPPER SILL REPAIRS IAW EA NR 7-5310-143936 AND EA NR 7-5310-143935.SDR FDEA201101160187Sill · misinstalledUPPER SILL BS 619 ON UPPER FLANGE HAS FASTENER WITH NO ED. ACCOMPLISHED MCD UPPER SILL REPAIR IAW EA 7-5310-143936, EA 7-5310-143935, & EA 7-5310-123575.SDR FDEA201101160185Sill · crackedUPPER SILL BS 502 NEAR UPPER FLANGE HAS CRACK INDICATION AT FASTENER HOLE. ACCOMPLISHED MCD UPPER SILL REPAIR IAW EA 7-5310-143936, EA 7-5310-143935, EA 7-5310-123575.SDR FDEA201101140176Skin · dentedSHARP DENT EXTERIOR FUSELAGE STA 500, STR 27R. CUT OUT DENT ON EXTERIOR SKIN IAW SRM 53-30- 3 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2 AND 53-30-3 FIG 1 REV. 103.SDR FDEA201101140175Vertical Beam · damagedAFT PIT, BS 1183, PRESSURE BULKHEAD VERTICAL BEAM HAS INSUFFICIENT SPACING AT LBL 17.8. ACCOMPLISHED REPAIR AT BS 1183 PRESSURE BULKHEAD VERTICAL BEAM IAW EA 7-5310-143934.SDR FDEA201012284757Controller · malfunctionedON TAKEOFF CLIMB AT 400'AGL, AT CLIMB POWER, EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. ENGINE ANTI-ICE WAS OFF, THE ENGINE RECOVERED AFTER A COUPLE OF BANGS, ALL ENGINE PARAMERTERS WERE NORMAL DURING CLIMB. WE OBSERVED NO OTHER ENGINE PARAMETERS DUSDR PCSA2010122101Clamp · looseNUMBER 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. MAINTENANCE RETORQED THE BLEED AIR HEAT EXCHANGER CLAMP, PERFORMED A LEAK AND OPERATIONAL CHECK ON AN ENGINE RUN-UP.SDR FDEA201012144661Duct · damagedON DESCENT, WITH WING ANTI ICE ON, RECEIVED LOWER AFT BODY LIGHT, WITH LOST AUTO PRESSURIZATION. RAN QRH, RESET WING ANTI ICE & TRIED AGAIN. RECEIVED LOWER AFT BODY LIGHT & AUTO PRESSURIZATION FAIL LIGHT AGAIN. RAN PRESSURIZATION IN MANUAL. TRIED AUTO PRESDR FDEA201012024536Control Handle · malfunctionedTHE AFT AIR STAIR LIGHT ON S/O PANEL CAME ON AT 1000FT ON TAKEOFF AND STAYED ON DURING DESCENT THE AFT AIR STAIR LIGHT WENT OUT AT LF 090 AND CAME BACK ON AT 4000 FT. RELEASED FOR SERVICE IAW MEL: 52-06-B. WORKED IN CONJUNCTION WITH TSI 52-30/4231. R & SDR PCSA2010120101Warning Light · illuminatedNR1 STRUT OVERHEAT LIGHT ILLUMINATED AT 33,000 FT. CLOSED NR 1 POWER LEVER AND LIGHT EXTINGUISHED. MX OPENED NR 1 PYLON, PRESSURIZED PNEUMATIC SYS CHECK FOR LEAKS, NONE NOTED IAW AMM 36-00-00. PERFORMED ENGINE RUN-UP AT PART POWER AND TAKEOFF. NO DEFECT NOTESDR FDEA201011294514Shear Tie · corrodedCORROSION - FRAME SHEAR TIE FORWARD FLANGE, STATION 1148, STRINGER 27L TO STRINGER 26L. REMOVED CORROSION FROM SHEAR TIE WITH A MATERIAL LOSS OF .004, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1. TREATED AND PRIMED AREA IAW SRM 51-10-2.SDR FDEA201011234480Stringer · corrodedCORROSION - INSIDE CHANNEL, STRINGER 22R, FWD SIDE OF STA 1166 FRAME. REMOVED SECTION OF STRINGER 22R, 23" IN LENGTH IAW SRM, REV 103, 53-10-3, FIG 1. FABRICATED STRINGER SECTION USING BAC1498-144, 7075-T6, 23" IN LENGTH AND STRAP USING 2024-T3, .125" X 1" X SDR FDEA201011234479Shear Tie · corrodedCORROSION - FWD LOWER FLANGE OF FRAME 950B, SHEAR TIE, BETWEEN STRINGER 30 AND STRINGER 29R. CUT OUT DAMAGED AREA OF SHEAR TIE IAW SRM, REV 103, 53-10-4, FIG 12. FABRICATED SHEAR TIE, & FILLER IAW SRM 53-10-4, FIG 12 AND 53-10-2, FIG 5. INSTALLED SHEAR TIESDR FOTR2019813712Seat Track · corrodedSEAT TRACK IS CORRODED AT LBL 24. CA/ REMOVED DAMAGED SEAT TRACK FROM STA 950+10 TO 1130 LBL 24 IAW SRM 51-30-2. FAB NEW SEAT TRACK FROM BAC1520-792-T65 PO NR 90010566 DIM. 25' LONG. LOCATED & DRILLED AREA & SEAT TRACK, TREATED AND PRIMED SEAT TRACK INSTALLED SDR FDEA201011174409Actuator · failedNR7 LED WOULD NOT RETRACT ON CLIMBOUT. RAN QRH AND IT WOULD NOT CLEAR. REPLACED THE NR 7 SLAT ACTUATOR WITH AND OVERHAULED UNIT PER MM 27-81-032-4. OPS CHECK AND LEAK CHECK GOOD. LEAK AND OPS CHECK NORMAL PER MM 27-81-032-4.SDR FDEA201011124321Switch · malfunctionedPANEL AFT STAIR AMBER LIGHT ILLUMINATED AFTER T.O AMBER AFT AIRSTAIR DOOR WARNING LIGHT - INOP. COMPLIED WITH MTSI 52-62/4199, INSPECTED BOTH THE UPPER AND LOWER CONTROL HANDLE MECHANISMS, CONTROL HANDLE DETENT SW S395, PULLEYS, HINGE POINT, MOUNTS AND NSDR PCSA2010111601Overheat Sys · false activationNR 1 STRUT OVERHEAT. PERFORMED ABNORMAL PROCEDURE. NO FURTHER OCCURRENCE. MAINTENANCE PERFORMED TEST OF THE OVERHEAT SYSTEM PER AMM. TEST NORMAL. ACCOMPLISHED ENGINE RUN-UP, SYSTEM CHECK NORMAL. NO OVERHEAT NR 1 ENGINE.SDR PCSA2010110501Warning System · activatedNR 1 STRUT OVERHEAT LIGHT ILLUMINATED DURING CRUISE WITH ENGINE ANTI-ICE ON. WHEN THE ANTI-ICE WAS TURNED OFF THE LIGHT WENT OUT.SDR PCSA201010210Warning Light · illuminatedLOG ITEM LEFT ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. REDUCED THRUST LEVER PER PROCEDURE. LIGHT EXTINGUISHED AFTER APPROX 30 SECONDS. RETURNED TO MIA. MAINTENANCE REMOVED THE PYLON PANELS. PERFORMED LEAK CHECK. NO LEAKS NOTED. PERFORMED ENGINE RUN-UP ASDR FDEA201010114002Contact · dirtyCABIN ENTRY EMERGENCY EXIT LIGHT DOES NOT TEST FROM COCKPIT SWITCH. REMOVED LIGHT ASSY CLEANED CONTACTS AND REINSTALLED IAW 33-50-101-2-0. OPS CHECKED GOOD. OK FOR SERVICE. REMOVED LIGHT ASSY CLEANED CONTACTS AND REINSTALLED IAW 33-50-101-2-0. OPS CHECKED GOSDR FDEA201010063955Duct · failedENGINE FAIL LIGHT ILLUMINATED AT 100 KTS ON T/O OAT 10. 169,000 TOGW. REJECTED T/O CHECKLIST COMPLIED WITH. R & R NR 2 ENGINE N1 GAUGE AS PRECAUTIONARY IAW AMM 31-00-011-4. RAN NR 2 ENGINE IAW JRH CHAPTER 6, ALL ENGINE PARAMETERS WERE NORMAL. ON RETURN TO SDR FDEA201009283775Engine · failedLOUD BANG/ ACFT SHUDDER DURING TAKEOFF, ACFT TAKEOFF REJECTED AT 115 KNOTS. GROUND PERSONNEL REPORTED HEARING 3 DISTINCT LOUD BANGS, NO APPARENT ENGINE MALFUNCTION NOTED PRIOR TO REJECT (ON GAUGE) WITH ALL INDICATIONS NORMAL AT IDLE. INSPECT ALL THE ACFT AISDR PCSA2010092701Rod · brokenNOSE LANDING GEAR DOOR DID NOT CLOSE WHEN GEAR WAS RETRACTED.SDR FDEA201009223652Battery Pack · inoperativeDURING PRE-DISPATCH CHECKS FOUND FWD ENTRY DOOR ESCAPE LIGHT INOP. DEN R RELEASED FOR SERVICE IAW MEL: 33-16-02-A CATEGORY: B EXPIRATION: 24SEP10 "MEL 33-16-02-A: FWD ESCAPE SLIDE LIGHT - INOP." L/E-LAMPED IAW SMP NO HELP.ITEM IS DEFFERED. R & R EMERGENCY SDR PCSA2010083001Tube · leakingNUMBER 1 ENGINE OIL QUANTITY STEADILY DECREASED DURING FLIGHT. ALSO OIL TEMP EXCESSIVE. ONLY DROPPED DURING POWER BACK. MAINTENANCE FOUND THE NUMBER 6 BEARING OUTER TUBE ON NUMBER 1 ENGINE LEAKING. THE TUBE PART NUMBER 793651 WAS REPLACED AND THE AIRCRAFT SDR PCSA2010072201Battery · dischargedPASSING THROUGH 3000 FT THE LOWER AFT CARGO FIRE ALARM SOUNDED. UPON LANDING MAINTENANCE PERFORMED OPS CHECK OF THE LOWER CARGO COMPT SMOKE DETECTION SYSTEM. FOUND NORMAL PER SECRURAPLANE CMM. NO FREIGHT IN AFT CARGO COMPT. PERFORMED VISUAL INSPECTION OF CSDR FDEA201007212633Valve · failedON CLIMBOUT NOTICED NR 1 OIL TEMP IN YELLOW RANGE. RAN THE QRH AND AFTER 15 MINUTES WE SHUT DOWN THE NR 1 ENGINE PER THE QRH. OPERATED NR 1 ENG FUEL HEAT SWITCH VALVE NO INDICATION NOTED.VISUALLY CHECKED FUEL HEAT VALVE, FOUND OPEN.REMOVED AND REPL ACED VSDR FDEA201007192596Structure · crackedRT WING, INBD FLAP, MID FLAP, AFT CHORD IS CRACKED AT WBL 112. CUTOUT SECTION CHORD CRACKED AT RT WING INBD FLAP MIDFLAP WBL 112 DIM: 47.6250" IAW SRM 51-40-4, FIG 1 AND FABRICATED SECTION CHORD FROM BAC 1503100046 7075T6 DIM: 47.6250 " & SPLICE DIM: 8.5" IAW SDR FDEA201007162566Skin · gougedSURROUND INNER SKIN GOUGED STA 620 STR 16L, CUT OUT DAMAGED AREA DIM APPROX 2" X 1" AND 1" X 1.2". FABRICATED DOUBLER REPAIR FROM 2024-T3 .125, DIM APPROX 9.50" X 4" AND FILLERS FROM 2024-T3, .125 DIM APPROX 2"X .950 AND 1.20" X .950 AND INSTALLED DOUBLER ANSDR FDEA201007152534Web · corrodedLH W/W CORROSION ON WEB AT STRINGER 18A FROM BS 920 TO 930 REMOVED SILL (WEB SHELF ON STRINGER 18A) AT BS 870 TO BS 950 LBL 55, FABRICATED SILL (WEB) FROM 7075O .080 DIM: 8.5" X 65.4, HEAT TREATMENT INSP 7075O TO T6 CONDITION IAW FASI REPORT 2-37153-801 REV A,SDR FDEA201007152556Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 990 BETWEEN STRINGERS 29L AND 28L CUT OUT DAMAGED SECTION OF SHEAR TIE 1" X 6" IAW FED SRM, REV 103, 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR USING 7075-0, .080" X 6" X 8.5" IAW SRM 53-10-4, FIG 15. INSTALLED SHEAR TIE REPAIR ISDR FDEA201007142561Skin · gougedSURROUND INNER SKIN GOUGES STA 640 STR 16L COMPLIED WITH EA 7-5330-135570 FUSELAGE AD 98-11-03 R1, SURROUND STRUCTURE, INNER SKIN GOUGE REPAIR BY BLENDING GOUGES IAW SRM 727 51-10-01 AND EA 7-5330-135570 AND FOUND WITHIN LIMITS EA 7-5330-135570.SDR FDEA201007132500Stringer · corrodedCORROSION ON STR 28L AT STRINGER SPLICE BS 1015.SDR FDEA201007122492Bulkhead · crackedMAIN CABIN 1183 BULKHEAD SKIN HAS CRACK AT LBL 60, WL 220 REMOVED LINE SUPPORT ANGLE, HORIZONTAL STIFENERS, CUT OUT DAMAGED AREA APPROX. DIM 4.29"X2.4", FABRICATED DOUBLER FROM P/N 2024-T3 .063 DIM 10 3/4" X 10", FABRICATED FILLER FROM P/N 2024T3 .050 DIM 2 3/SDR FDEA201007092441Skin · gougedMCD SURROUND INNER SKIN GOUGED STA 460 STR 5L. REMOVED INNER SKIN BS 460-510 UPPER FWD IAW SRM 51-30-2. FABRICATED INNER SKIN FROM 2024 T3 .125" PO 90010048 DIM: 48" X 79" IAW DRAWING 53FX2022 REV C. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED FWD UPPER INSDR FDEA201007092464Seat Track · corrodedSEAT TRACK CORRODED MAIN CABIN LBL 45 BS 850-760. REMOVED DAMAGED SEAT TRACK AND "T" CHORD AND FABRICATED NEW SEAT TRACK FROM BAC 1520-3417178T6 AND NEW "T" CHORD FROM BAC 1506-1108-7075T6. INSTALLED NEW SEAT TRACK & "T" CHORD ALL IAW DWG 65-16279 & SRM 51-3SDR FDEA201007092440Skin · gougedSURROUND INNER SKIN GOUGED STA 620, STR 5L. REMOVED INNER SKIN 600 TO 640 UPPER AFT IAW SRM 51-30-2. FABRICATED INNER SKIN FROM 2024T3 .125 DIM 48" X 79" IAW DRAWING 53FX2022. INSTALLED NEW INNER SKIN IAW SRM 51-30-2.SDR FDEA201007092442Skin · gougedSURROUND INNER SKIN GOUGED STA 520, STR 5L. REMOVED MAIN CARGO DOOR INNER SKIN CENTER AREA IAW SRM 51-30-2. FABRICATED CENTER INNER SKIN USING 2024 T3 .090" PO 2011153 DIMENSIONS 88" X 34" IAW DWG 53FX2022. TREATED AND PRIMED INNER SKIN IAW SRM 51-10-2. INSTSDR FDEA201007092466Skin · delaminatedRT WING INBD AILERON TAB HAS DISBONDING T/E SKIN SURFACE REMOVED DAMAGED AREA (15.5" X 3.52") SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-00 PARAGRAPH NR 7. FABED FILLER AND DOUBLER ( 15.5" X 3.5") AND DOUBLER (19" X 5.5") FROM 2024T3 .012 IAW SRM 51-40-20 SDR FDEA201007082474Support Angle · crackedRT LOWER TORQUE BOX UPPER SUPPORT ANGLE IS CRACKED AT INBD END BS 1263 REMOVED RT LOWER TORQUE BOX UPPER SUPPORT ANGLE IAW SRM 51-30-2, FABRICATED UPPER SUPPORT ANGLE MATERIAL USED BAC 1514-1617 7075 T6511 PO NR 20105119 DIM 28" X 3.2500" IAW DWG NR 65-1
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