Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 CALA9802076Cover · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER T/E HINGE COVER OF NR 3 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-20-1 AND 51-30-2, PARAGRAPH 7.SDR CALA9802075Cover · crackedINSPECTION FOUND A .1875 AND .125 CRACK IN LT WING UPPER T/E HINGE COVER OF NR 2 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-30-2, PARAGRAPH 7.SDR CALA9802074Web · puncturedINSPECTION FOUND A PUNCTURE IN FORWARD CARGO AREA WEB JUST FORWARD OF UPPER AFT DOOR STOP. THE PUNCTURED AREA WAS ROUTED OUT IAW SRM 51-10-1, PAGE 6B. A WEB REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-10-2, PAGE 4.SDR CALA9802073Bracket · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN NR 6 LE FLAP O/B ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-20-1, FIGURE 18.SDR CALA9802072Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING NR 2 SLAT LOWER CHORD ANGLE BELOW TELESCOPING ANTI-ICE DUCT AREA. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, PAGE 16.SDR CALA9802071Plate · crackedINSPECTION FOUND A 1 INCH CRACK IN PLATE AT RT INBOARD MIDFLAP ABOVE AFT END OF NR 5 SPINDLE. THE PLATE WAS REMOVED IAW SRM 51-30-2, PAGE 4. A NEW PLATE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2, PAGE 1.SDR CALA9802070Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT SCREW HOLE TO RIVET HOLES OF NR 2 SLAT UPPER TRAILING EDGE WHERE I/B HOOK MOUNTS. THE FASTENERS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 3 AND 57-50-3, PAGES 27-28.SDR CALA9802069Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN SKIN AT AFT FACE OF LT WING NR 1 SLAT, INBOARD OF INBOARD TRACK AREA. THE NR 1 LE SLAT WAS REMOVED AND REPLACED IAW MM 27-81-11.SDR CALA9802068Skin · corrodedINSPECTION FOUND LT FUSELAGE SKIN BULGED JUST BELOW AND AFT OF LAV SERVICE PANEL CUTOUT AREA AT BS 1191, S21L TO S22L. THE AREA WAS REPAIRED IAW SRM 53-30-3 AND BOEING SERVICE BULLETIN 727-0550048.SDR DL72S982375Light · inopEMER AREA LIGHT AT WING EXITS IN CABIN INOP. FOUND THAT LAMP AT EXTERIOR WING EXIT SHORTING CIRCUIT. REPLACED LAMP AND BATTERY PACK AND RACK FUSES, OPERATION CHECK GOOD.SDR DL72L982374Battery Pack · dischargedRIGHT AFT EMERGECY OVERWING LIGHTS ON AFT CARGO DOOR INOP. REPLACED BATTERY PACK.SDR DL72S982360Light · inopL2 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY.SDR DL72S982355Battery Pack · dischargedAFT SERVIVCE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY RACK.SDR DL72S982354Battery · dischargedAFT GALLEY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY.SDR DL72S982353Megaphone · inopMEGAPHONE INOP. REPLACED MEGAPHONE.SDR DL72L982358Battery · dischargedAFT AIRSTAIR EMERGENCY LIGHTS FAILED TO TEST. REPLACED BATTERY.SDR DL72L982350Light · inopL-1 AND FWD AISLE AREA EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN THE L-1 DOOR POS AND REPLACED LIGHT ASSY FOR THE FWD AISLE EMERGENCY LIGHT.SDR DL72K982356Power Supply · inopFWD FLOOR EMERG LIGHTS INOP. REPLACED POWER SUPPLY.SDR CALA9802065Battery · dischargedINSPECTION FOUND THE AFT FLIGHT ATTENDANT STATION LOWER FLASHLIGHT WEAK. THE FLASHLIGHT BATTERY WAS REPLACED IAW MM 25-20-0.SDR CALA9802064Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN E & E COMPARTMENT DOOR FRAME BEHIND RIGHT STOP FITTING. THE DOOR ASSEMBLY WAS REPLACED IAW MM 52-40-11.SDR CALA9802063Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN SPAR ATTACH ANGLE OF RT WING LEADING EDGE RIB AT WS 115. THE CRACK WAS STOP DRILLED IAW SRM 51-40-3. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9802062Chord · corrodedINSPECTION FOUND RT WING LOWER CHORD CORRODED AT WS 645 TO 636. THE CORROSION WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2, PAGE 14, 51-10-2, PAGE 4 AND 51-30-10 PAGE 1.SDR CALA9802061Web · crackedINSPECTION FOUND A 4 INCH CRACK IN MAIN ENTRY L-1 DOOR WEB AT TOP AFT CORNER OF DOOR. THE CRACKED AREA WAS REMOVED. A MOUNT AND RIB WERE INSTALLED IAW SRM 51-10-1, 51-10-2 AND 51-30-2, PAGE 2-7.SDR CALA9802060Floorbeam · corrodedINSPECTION FOUND COCKPIT FLOORBEAM CORRODED AT STA 242 FORWARD OF RT GEAR MANUAL EXTENSION. SUPPORT BRACKET AND FASTENERS WERE REMOVED AND A NEW BRACKET AND ANGLE SUPPORTS WERE INSTALLED IAW SRM 53-10-8 PAGE 52 AND 51-10-2 FIGURE 4.SDR DL72S982341Stop · looseDURING INSPECTION PER REQUIREMENTS OF AD 94-07-08, LOOSE SLAT STOP ATTACH BOLTS WERE FOUND LOOSE FOR THE NR 6, 7 & 8 SLATS. EACH OF THESE SLAT LOCATIONS WERE MODIFIED PER THE REQUIREMENTS OF BAC S/B 727-57-171. THE MODIFICATION WAS DOCUMENTED PER ER/A 366092SDR DL72S982339Battery Pack · dischargedRIGHT AFT OVERWING EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.SDR DL72S982329Frame · crackedFOUND AT LETTER CK B-2, AFT ENTRY DOOR CUTOUT LT FRAME HAS .3125 INCH VISIBLE CRACK 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-8.SDR DL72S982324Angle · crackedLWR CHORD ANGLE 1 INCH CRACK AT FWD END BELOW NR 8 SPOILER ACTUATOR. REPAIRED PER M/M 57-20-22 FIG 806.SDR DL72S982323Bracket · crackedNR 6 L/E FLAP ACT ATTACH BRACKET CRACKED AT UPPER AND LWR ENDS. REPAIRED PER M/M 57-20-21 FIG 807.SDR DL72S982322Skin · crackedA .375 INCH CRACK AT NR 2 MIDFLAP LOWER SURFACE AT CUTOUT I/B OF NR 4 MIDFLAP FAIRING. REPAIRED PER M/M 57-52-0.SDR CALA9802053Skin · dentedINSPECTION FOUND RT OUTBOARD AILERON TAB DENTED. THE RT OUTBOARD AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-0.SDR CALA9802052Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 720C, RBL 2 WITH A HOLE CHAFED THROUGH AT LBL 6. THE CRACKED AND CHAFED AREAS WERE CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND BOEING DRAWING 7275331041.SDR CALA9802051Casting · crackedINSPECTION FOUND A 1.62 INCH CRACK IN LT WING NR 3 LEADING EDGE FLAP MAIN CASTING AT O/B HINGE MOUNT AREA. THE NR 3 LEADING EDGE FLAP WAS REMOVED AND REPLACED IAW MM 27-81-1.SDR DL72S982299Power Supply · inopFIRST CLASS EMERGENCY LIGHTS INOP. REPLACED BATTERY PWR SUPPLY, NOW CKS GOOD.SDR DL72S982298Battery · dischargedEMERGENCY LIGHTS L2 DOOR DID NOT TEST ON LAYOVER. REPLACED BATTERIES, NOW TESTS NORMAL.SDR DL72S982290Angle · crackedHORIZ TORQUE BOX ANGLE CRACKED STA 1263 BELOW FWD END OF ACTUATOR PAD. HORIZ GUSSET ANGLE CRACKED STA 1263 BELOW ACTUATOR PAD. REPLACED ANGLE AND GUSSET PER SRM 53-10-10 FIG 1-3.SDR DL72S982287Coffeemaker · failedELECTRICAL BURNING SMELL EMITTING FROM F/C GALLEY. REPLACED F/C COFFEEMAKER AND CANNON PLUG.SDR DL72S982286Battery Pack · weakON PREFLIGHT, CREW REPORTED AFT EMER EXIT LIGHT FLASHING. REPLACED BATT PACK, OPER OK.SDR DL72S982282Rib · crackedDURING SHOP INSPECTION, A REPAIR DOUBLER AT THE I/B AFT RIB WAS FOUND TO BE CRACKED. THE DOUBLER WAS REMOVED AND THE RIB WAS REPAIRED PER MM 57-52-0 FIG 808.SDR DL72S982567Spar · crackedNR 2 MID FLAP, CRACK AFT SPAR RAIL 33 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 615732.SDR DL72S982301Flap Track · corrodedINBOARD FLAP INBOARD TRACK TYP CORROSION AT FWD LUG AND MLG BEAM ATTACH HOLES: AD 90-07-05. INSTALL OVERSIZED BUSHINGS IN FWD LUG HOLES, OVERSIZE MLG BEAM ATTACH HOLES AND PROCEED WITH SPLICE PLATE REPAIR PER BAC SB 727-57-0178.SDR DL72K982304Skin · dentedTHE FUSELAGE SKIN WAS FOUND DENTED JUST ABOVE STRINGER 21R BETWEEN FS 1166 AND 1183. THE DENT WAS CUT OUT 2 X 7.25, REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366004-14, REV B.SDR CALA9802040Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STIFFENER INSIDE VERTICAL FIN ABOVE S DUCT AREA AT BS 1303-1323, BL 0. A NEW STIFFENER WAS INSTALLED IAW SRM 51-10-1, PAGE 2 AND 51-30-2, PAGE 4.SDR DL72S982404Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 19 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.SDR DL72S982280Frame · crackedDURING C-1 LETTER CHECK, .5 INCH VISIBLE CRACK IN AFT ENTRY DOOR CUTOUT LT FRAME AT SECOND FROM UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.SDR DL72S982273Rib · crackedFOUND ON C1 LETTER CK, NR 4 SLAT L/E NOSE RIB I/B SIDE OF ACTUATOR CRACKED .5 INCH. REPAIRED PER MM 57-54-0.SDR DL72S982272Angle · crackedFOUND ON C1 LETTER CK, STA 913 ANGLE CRACKED O/B END OF LT WHEEL WELL. REPAIRED PER MM 53-11-0.SDR DL72S982271Frame · crackedFOUND AT C1 LETTER CK, .5 INCH VISIBLE CRACK IN AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER STOP CASTING. REPAIRED PER SRM 53-10-9 FIG 11.SDR CALA9802039Support · crackedINSPECTION FOUND A .5 INCH CRACK IN RT HORIZONTAL STABILIZER TRAILING EDGE ELEVATOR AT STA 99.79 ATTACHING HINGE SUPPORT. THE ATTACHING HINGE SUPPORT WAS REPAIRED IAW SRM 55-10-4, PAGE 10-13 AND 51-30-2, PAGE 10.SDR CALA9802038Skin · delaminatedINSPECTION FOUND RT WING O/B TE AFT FLAP O/B END UPPER SURFACE DELAMINATED AT SPAR. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
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