Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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 = '727224' 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 CALA9800818Bracket · crackedLT MLG WALKING BEAM PANEL HAS BROKEN ATTACH BRACKET (1/2 CRACK) I/B END OF PANEL. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.SDR CALA9800806Rib · crackedFIRST RIB AFT OF AFT ENG MOUNT IS CHAFED TWO SPOTS NUMBER ONE ENGINE PYLON. REMOVED DAMAGED AREA NR 1 ENGINE PYLON MOUNT RIB. FABRICATED NEW REPAIR, INSTALLED PER SRM 51-40-2 AND 51-30-2.SDR CALA9800805Apron · crackedNUMBER ONE ENGINE AFT APRON HAS DAMAGED SKIN CAUSED BY CHAFING ON FORWARD STIFFENER. FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR PER SRM 51-10-2, 54-10-3, 51-30-2, AND MM 51-20-11.SDR CALA9800804Apron · crackedNUMBER 1 ENGINE FORWARD APRON CRACKED (2) ON UPPER SIDE. REMOVED DAMAGED, INSTALLED DOUBLER AND FILLER PER SRM 51-40-2 AND 51-30-2.SDR CALA9800803Gearbox · crackedNUMBER 2 ENGINE GEARBOX DATA PLATE MOUNT BOLT HOLE (UPPER AFT) BROKEN OUT. REPAIRED GEARBOX DATD PLATE MOUNT BOLT HOLE PER EC/RA 7261-01251.SDR CALA9800802Angle · corrodedFS 950 RT ELEPHANT EAR FAIRING ATTACH ANGLE HAS CORROSION ON UPPER AND LOWER FLANGES. CUT OUT SECTION OF ATTACH ANGLE FABRICTED FILLER AND ANGLE. TREATED, PRIMED AND INSTALLED ANGLES PER SRM 51-10-6, 53-10-6, 53-10-1, 51-40-4 51-30-2, AND 57-40-4.SDR CALA9800785Trunnion · corrodedRIGHT MLG FORWARD TRUNNION ATTACH FITTING AIRCRAFT SIDE HAS CORROSION ON INNER FACE OF BOTH I/B AND O/B ATTACH FITTINGS AROUND BUSHINGS BOTH UPPER AND LOWER HOLES. REMOVED CORROSION, REAMED HOLES, FABRICATED AND INSTALLED BUSHINGS PER BOHM 32-10-13 AND BSOP 2SDR CALA9800784Trunnion · corrodedLEFT MLG FORWARD TRUNNION FITTING HAS CORROSION AROUND BOTH LOWER BUSHINGS INNER SIDES AND I/B SIDE OF FITTING UPPER BUSSING INNER SIDE. REAMED HOLES AND FABRICATED TWO BUSHINGS PER BOHM 32-10-13.SDR CALA9800783Trunnion · gougedLEFT MAIN LANDING GEAR FORWARD TRUNNION FITTING O/B SIDE OF FITTING BOTH UPPER AND LOWER BUSHING ARE GOUGED. REAMED HOLE AND FABRICATED 2 BUSHINGS PER BOHM 32-10-13 FIGURE 3.SDR CALA9800782Panel · corrodedFORWARD PIT LT TRANSITION PANEL STA 620 TO 580 HAS CORROSION. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-2, 51-10-2, AND MM 51-20-11.SDR CALA9800781Step · corrodedAFT AIRSTAIRS NR 8 STEP PANEL CORRODED. REMOVED CORRODED AREA, FABRICATED, TREATED AND INSTALLED REPAIR SECTION PER SRM 51-40-2, 51-10-2 AND MM 51-20-11.SDR CALA9800780Panel · corrodedTRANSITION PANEL AFT PIT STA 950 TO 970 LT SIDE CORRODED ON UNDER SIDE OF PANEL. REMOVED CORRODED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS PER SRM 51-10-6, 53-10-1, 51-4-0-2, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800779Fairing · corrodedLOWER SKIN FAIRING AT STA 950 IS CORRODED BEYOND LIMITS. FABRICATED, TREATED, PRIMED, AND INSTALLED NEW LOWER SKIN FAIRING PER SRM 51-40-2, 51-10-2 AND MM 51-20-11.SDR CALA9800778Access Panel · corrodedLT LOWER HORIZ STAB BAL BAY ACCESS PANEL CORRODED. CUT OUT CORRODED AND DELAMINATED AREA, FABRICATED DOUBLER AND BONDED TO CUT OUT AREA PER SRM 55-20-3 AND 51-40-5.SDR CALA9800755Light · inoperativeAFT AIRSTAIRS EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT PER MM33-50-61.SDR CALA9800754Apron · crackedNUMBER ONE ENGINE FORWARD APRON CRACKED AT RIVET HEAD IN LOWER AFT CORNER (.5). REMOVED CRACKED DOUBLER. FABRICATED, TREATED, PRIMED, AND INSTALLED DOUBLER AFTER REMOVING CRACKED AREA PER SRM 51-40-2, 51-10-2, AND MM 51-20-11.SDR CALA9800753Access Panel · delaminatedHORIZ STAB ELEVATOR PCU ACCESS PANEL DELAMINATED 3 X 10. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND BONDED TO PANEL PER SRM 55-20-3 AND 51-40-5.SDR CALA9800752Support · corrodedFLOOR SUPPORT AT STA 535 LBL 8 OUT OF LIMITS. FORMED ANGLE FROM 7075-0 PER SRM 51-40-3. HEAT TREAT PER BCA 5602. TRATED, PRIMED AND INSTALLED PER SRM 51-10-2, 51-40-3, AND MM 51-20-11.SDR CALA9800735Support · corrosionAFT PIT STA 1166 FLOOR SUPPORT IS OUT OF LIMITS AT RBL 5. CUT OUT AREA, FABRICATED REPAIR, TREATED, PRIMED AND INSTALLED PER SRM 53-105, 51-10-2, 51-30-2 AND 51-20-11.SDR CALA9800734Light · inoperativeR1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED R1 EMERGENCY LIGHT ASSY PER MM 33-50-91.SDR CALA9800731Fitting · corrodedAFT PIT FS 1183 STR 30 AFT JACK PAD MOUNT CORRODED BEYOND LIMITS. DRILLED, DEBURRED, TREATED, AND PRIMED NEW MOUNT AND NEW INTERCOSTAL PER SRM 51-30-5, 51-10-2, AND MM 51-20-11. INSTALLED NEW MOUNT AND INTERCOSTAL PER SRM 51-30-2. INSTALLED E/Q BAFFLE PER SRSDR CALA9800733Isolator · slippedNUMBER 2 ENGINE FORWARD MOUNTS HAVE EVIDENCE OF SLIPPAGE AND DISBONDING. REPLACED NUMBER 2 ENGINE FORWARD ISOLATORS PER MM 71-21-1.SDR CALA9800732Support · gougedAFT CARGO PIT FLOOR SUPPORT GOUGE AT STA 1007 LBL 15. REMOVED GOUGED AREA, FABRICATED NEW PART AND DOUBLERS AND INSTALLED PER SRM 51-40-4.SDR CALA9800730Support · corrodedAFT PIT STA 1166 FLOOR SUPPORT IS OUT OF LIMITS AT RBL 5. CUT OUT AREA. FABRICATED REPAIR, TREATED, PRIMED AND INSTALLED PER SRM 53-10-5, 51-10-2, 51-30-2 AND MM 51-20-11.SDR CALA9800713Chord · corrodedINSPECTION FOUND LOWER RT T-CHORD CORRODED AT FS 950. THE CHORD WAS REMOVED. A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, PAGE 4, PARAGRAPH 4 AND SRM 51-30-2.SDR CALA9800712Stringer · corrodedINSPECTION FOUND STRINGER 28L AND STRINGER TIE CORRODED AT FS 950. THE STRINGER TIE AND CORRODED END OF STRINGER WERE REMOVED. REPAIR WAS INSTALLED IAW SRM 51-10-2, 53-10-3, AND MM 51-20-11.SDR CALA9800710Support · crackedINSPECTION FOUND A 6.5 CRACK IN FLOOR SUPPORT AT STA 485, LBL 12. THE CRACKED SECTION WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800709Floor Support · crackedINSPECTION FOUND A 10.75 CRACK IN FLOOR SUPPORT AT STA 680, RBL 24. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 1, 51-10-2, AND MM 51-20-11.SDR CALA9800708Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT RBL 8 AND LBL 13, STA 535. THE CORRODED AREAS WERE CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-20-11.SDR CALA9800707Support · corrodedINSPECTION FOUND FLOOR SUPPORTS AT RBL 2 AND LBL 2, STA 535 CORRODED. THE CORRODED AREAS WERE CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-36, 51-10-2, 51-30-2, 51-40-3, FIGURE 1, AND MM 51-20-11.SDR CALA9800706Clip · corrodedINSPECTION FOUND STRINGER TIE CLIP CORRODED AT FS 950E. THE CLIP WAS REMOVED AND A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800705Intercostal · crackedINSPECTION FOUND A 5 CRACK WITH CORROSION IN INTERCOSTAL FOOT BETWEEN STRINGERS 29R AND 28R AT STA 950E. THE CRACKED AND CORRODED AREA WAS CUT OFF IAW SRM 53-10-4. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800704Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT LBL 12 AND LBL 4, STA 1166. THE CORRODED SECTIONS OF FLOOR SUPPORT WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-5, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800703Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1166, RBL 16. THE CORRODED AREA WAS CUT OUT. A CHANNEL AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11.SDR GAIA9837Indicator · looseAFTER DEPARTURE FROM IAH-TOL, THE INBOARD FLAPS FROZE AT 2 DEGREES. AIRCRAFT RETURNED TO IAH. AFTER 10 MINUTES FLAPS WENT TO 30 DEGREES, BUT ON TAXI IN FLAPS FROZE AT 2 DEGREES AGAIN. THE FLT CREW DECLARED AN EMERGENCY INTO IAH AND MADE AN UNEVENTFUL LANDINSDR CALA9800586Battery Pack · dischargedINSPECTION FOUND CEILING EMERGENCY EXIT LIGHT BETWEEN R-2 DOOR AND L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR 98ZZZX1362Valve · failedAIRFCRAFT UNDERGOING 4B CHECK, HYDRAULIC SHUT-OFF VALVE TO NR 2 ENGINE WOULD NOT OPERATE. WHEN NR 2 ENGINE FIRE PULL T-HANDLE WAS PULLED, THE CIRCUIT BREAKER FOR THE HYDRAULIC SHUT-OFF VALVE TRIPPED. TROUBLELSHOOTING REVEALED THE VALVE WAS STUCK IN THE OPEN SDR CALA9800398Retract Mech · out of rigTHE NOSE GEAR DOORS CAME OPEN ACCOMPANIED BY ILLUMINATION OF THE RED NOSE GEAR DOORS LIGHT WITH THE GEAR HANDLE IN UP OR OFF POSITION WHILE AT CRUISE. VIBRATION WAS FELT AND NOISE LEVEL HAD INCREASED. MAINTENANCE FOUND THE NOSE GEAR DOORS OUT OF RIG. THE DOSDR CALA9800386Turbine · failedTHE NR 3 ENGINE OIL PRESSURE WENT TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE EN ROUTE FROM RSW TO EWR. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND RSDR 98ZZZX1688Metering Valve · crackedWHILE BEING OVERHAULED, AN OCCURRENCE OF CRACKS WERE NOTED IN SEVERAL VALVE BODIES. THERE ARE NO NDT CHECKS FOR BODY P/N 1692E41 OTHER THAN X10 MAGNIFICATION VISUAL CHECK IN THE SARGENT OMM 32-50-04. SUBMITTER SUGGESTED THAT AS A MINIMUM, A DYE PENETRANT FLASDR CALA9800268Harness · chafedFIRE AND SMOKE OCCURRED IN THE LT AFT LAV WHILE EN ROUTE. A FIRE EXTINGUISHER WAS USED TO PUT OUT THE FIRE. THE ACFT LANDED AT IAH WITHOUT FURTHER INCIDENT. THE FIRE WAS CONTAINED WITHIN THE LAV. PRELIMINARY FINDINGS REVEALED THE WIRING TO THE LAV FLUSH TISDR CALA9800254Skin · crackedINSPECTION FOUND A .625 INCH CRACK AND TWO SHEARED FASTENERS IN LEFT WINGTIP LOWER TRAILING EDGE SKIN. THE FASTENERS WERE REMOVED AND THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-02.SDR CALA9800253Rib · crackedINSPECTION FOUND A 1.5 CRACK IN WINGTIP MOUNT RIB AT WINGTIP AREA AFT OF NAV STROBE LIGHT. AN ANGLE DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9800252Doubler · crackedINSPECTION FOUND A 2 INCH CRACK IN DOUBLER OF RT WINGTIP TRAILING EDGE AT WBL 626. THE WINGTIP WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. THE WINGTIP WAS REINSTALLED IAW SRM 51-30-2 AND MM 33-40-0.SDR CALA9800251Skin · debondedINSPECTION FOUND LT INBOARD FOREFLAP INBOARD TRAILING EDGE SKIN DEBONDED WITH CHAFE MARKS ALONG UPPER SURFACE. THE FOREFLAP WAS REMOVED, REPAIRED AND REPLACED.SDR CALA9800250Skin · crackedINSPECTION FOUND A 1.375 CRACK IN LT WING NR 4 SPOILER AT LOWER SKIN JUST INBOARD OF SECOND FROM INBOARD HINGE. THE NR 4 SPOILER WAS REMOVED AND REPLACED.SDR CALA9800232Casting · crackedINSPECTION FOUND A 1 INCH CRACK IN LT OUTBOARD FOREFLAP OUTBOARD END CASTING LOWER ATTACH LUG. THE LT OUTBOARD FOREFLAP VANE WAS REMOVED AND REPLACED IAW MM 27-50-00.SDR CALA9800231Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT WING NR 2 SLAT CHORD ANGLE BELOW WHERE INBOARD STOP PAD MOUNTS. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-01.SDR CALA9800230Skin · crackedINSPECTION FOUND SEVERAL .375 INCH CRACKS FROM FASTENER HOLE AT NR 4 SLAT UPPER SKIN WHERE INBOARD HOOK MOUNTS. TWO .375 INCH CRACKS WERE FOUND AT NR 4 SLAT UPPER SKIN WHERE OUTBOARD HOOK MOUNTS. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3.SDR CALA9800229Wire · brokenINSPECTION FOUND THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT CANNON PLUG. THE WIRE WAS REPAIRED AND THE BATTERIES WERE CHARGED.
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