Boeing 727-22C

Service difficulty reports · 2,328

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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 = '72722C'
  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.

SDR RAAAOOB2036Battery · dischargedDURING SERVICE CHECK, FOUND EXIT IDENTIFIER FAILED TEST AT ROW 14 ABC. REPLACED BATTERY AND TESTED IAW RAA GMM.Jun 29, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA00B2035Battery · dischargedDURING SERVICE CHECK, FOUND EXIT SIGN LIGHT FAILED TEST. REPLACED BATTERIES AND TESTED IAW RAA GMM.Jun 29, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR 00FDEA00412Flap · malfunctionedWHILE CONFIGURING FOR LANDING, FLAP HANDLE AT 25 DEGREES, INBD FLAP INDICATOR (FWD ONE) READ 0. DURING GO-AROUND WHEN FLAPS CONFIGURED TO 15, FWD INBD INDICATOR 15 & ALL INDICATORS WORKED NORMAL. RAN FLAPS THRU SEVERAL CYCLES OPS CHECK GOOD PER 27-52-000-0. Jun 27, 2000 · N103FE · Boeing 72722C · Trailing Edge Flap Control SystemSDR DHL2000706005Intercostal · crackedFWD RT LAV FLOOR FRAME INTERCOSTAL HAS 2 LARGE CRACKS EMINATING FROM TOP, LOCATED I/B OF DUMP SHUTE BS 303.9, RBL 43. REMOVED WEB FOR REPLACMENT PER SRM 57-30-2. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 53-10-1. TREATED WITH ALODINE AND PRIMED PER SJun 22, 2000 · N706DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2000706006Angle · brokenAFT CARGO COMPT APPROX BS 950 AFT AREA, WL 195.0 & BBL 0.0 ANTI ICE DUCT HAS ANGLE SUPPORT BROKEN AT LOWER SECTION. REMOVED AND INSTALLED NEW ATTACH ANGLE SUPPORT PER SRM 53-10-01. ALODINED AND PRIMED PER SRM 51-10-2.Jun 21, 2000 · N706DH · Boeing 72722C · Fuselage Main, Attach FittingsSDR DHL2000706004Threshold · corrodedFWD RT LAV FLOOR AT THRESHOLD HAS CORROSION ABOVE AND BELOW FLOOR BS 328, RBL 14. REMOVED THRESHOLD PER SRM 51-30-2. FABRICATED NEW THRESHOLD PER SRM 53-10-1. INSTALLED NEW THRESHOLD PER SRM 51-30-2.Jun 21, 2000 · N706DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2000706003Attach Angle · crackedFWD ENTRY DOOR PANEL (INTERIOR) AFT SUPPORT ATTCH ANGLE CRACKED SEVERAL PLACES. REMOVED AND REPLACED ANGLES PER SRM 51-30-2. TREATED AND PRIMED SUPPORT ANGLES PER SRM 51-10-2.Jun 21, 2000 · N706DH · Boeing 72722C · Passenger/Crew DoorsSDR DHL2000706002Floorboard · damagedFLOOR PANEL DAMAGED AT FWD LEFT CORNER AT BS 360 PANEL FROM RBL 24.0 TO 48.0. REMOVED FLOORBOARD, FABRICATED DOUBLERS PER SRM 53-20-1. ALODINED AND PRIMED PER SRM 53-20-1. INSTALLED FLOOR PANEL PER SRM 51-30-2.Jun 21, 2000 · N706DH · Boeing 72722C · Fuselage Floor PanelSDR RAAA00B2034Battery · dischargedDURING SERVICE CHECK, FOUND FLOOR PROXIMITY LIGHT WOULD NOT TEST AT ROW 15. REPLACED BATTERY. LIGHT TESTS GOOD PER RAA ECO 86-26.Jun 21, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR DHL2000705005Door · not closedON TAKEOFF ROLL, EQUIPMENT ACCESS DOOR LIGHT CAME ON. A/C WOULD NOT PRESSURIZE. RETURNED TO GVG. FOUND FWD E & E DOOR NOT LATCHED PROPERLY. INSPECTED DOOR LATCH MECHANISM, NO DEFECT NOTED. RESECURED DOOR, OPS CHKS GOOD PER M/M 52-40-1.Jun 13, 2000 · N705DH · Boeing 72722C · Electrical/Electronic Compartment DoorsSDR 20001011AP010Valve · failedFLT 744 - LAX - STRONG SMELL OF SMOKE IN COCKPIT DURING TAKEOFF ROLL AND CLIMB-OUT. AIR TURN BACK TO LAX. REPLACED 13TH STAGE MODULATION VALVE ON NR 1 ENGINE AND BOTH COALESSOR BAGS. (M)Jun 10, 2000 · N427EX · Boeing 72722C · Cabin Cooling SystemSDR 20000816AP002Engine · overheatedFLT 748 - OMA-IND - NR 2 ENGINE EGT WAS RAPIDLY APPROACHING RED LINE AT 1000 FEET ABOVE GROUND LEVEL. POWER WAS REDUCED EGT REMAINED IN THE YELLOW ARC. REPLACED NR 2 ENGINE. (M)Jun 9, 2000 · N428EX · Boeing 72722C · Engine (Turbine/Turboprop)SDR 00FDEA00378Spar · crackedDURING ROUTINE INSPECTION, RIGHT I/B MIDFLAP REAR SPAR UPPER CHORD FOUND CRACKED AT WING BUTT LINE 120 UPPER ROW FWD FASTENER HOLE. REMOVED AND REPLACED PER IAW MM 27-51-1. RIG AND OP CHECK FLAP PER IAW MM 27-51-0.Jun 5, 2000 · N101FE · Boeing 72722C · Trailing Edge FlapsSDR 00FDEA00377Floorbeam · corrodedDURING ROUTINE INSPECTION, FLOORBEAM BS 640 FOUND CORRODED BEYOND LIMITS 4 INCHES LEFT OF NR 4 SEAT TRACK. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-8.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 00FDEA00376Floorbeam · corrodedDURING ROUTINE INSPECTION, FLOORBEAM BS 344 FOUND CORRODED BEYOND LIMITS ON UPPER CHORD AT RBL 50. CUT OUT DAMAGE, FAB AND INSTALL PER IAW SRM 53-10-8.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 00FDEA00375Floorbeam · corrodedDURING ROUTINE INSPECTION, FLOORBEAM BS 344, RT O/B END FOUND CORRODED BEYOND LIMITS ON LWR FLANGE. CUT OUT DAMAGE. FAB AND INSTALLED PER IAW SRM 53-10-8.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 00FDEA00374Stringer · crackedDURING ROUTINE INSPECTION, STR 25R FOUND CRACKED BS 520. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-3.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 00FDEA00373Floorbeam · crackedDURING ROUTINE INSPECTION, LWR FLOORBEAM CORROSION AT BS 848 FROM RBL 0 - 24 AND CRACKED AT RBL 1. REMOVED CORROSION IAW SRM 51-10-6, STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE AND SUPPORT DOUBLER IAW 51-40-3 & 51-30-2.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 00FDEA00372Seat Track · corrodedDURING ROUTINE INSPECTION, BS 870 FLOORBEAM FOUND CORRODED AT THE NR 1 SEAT TRACK. REMOVED AND REPLACED PER IAW SRM 51-10-6. FOUND WITHIN LIMITS IAW SRM 53-10-1, 51-30-2.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00371Skin · corrodedDURING ROUTINE INSPECTION UPPER FUSELAGE SKIN FOUND CORRODED AND POPPED RIVETS FROM BS 430 - 440 AT STR 5L. REMOVED RIVET AND TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3. FAB REPAIR PARTS PER IAW SRM 53-30-3.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 00FDEA00370Support Bracket · crackedDURING ROUTINE INSPECTION, SUPPORT BRACKET FOR NR 7 SPOILER ACTUATOR FOUND CRACKED AT BOTH SIDES. REMOVED AND REPLACED NR 7 SPOILER AND ACTUATOR FITTING PER IAW SRM 51-10-1, 51-30-2, 27-62-001-4, AND 27-62-00. OPS CHECK GOOD.Jun 5, 2000 · N101FE · Boeing 72722C · SpoilersSDR 00FDEA00369Beltframe · crackedDURING ROUTINE INSP BS 930 BELTFRAME FOUND CRACKED ON FWD SIDE OF STR 14R. REPAIRED BELTFRAME PER IAW FEDEX EO 7-2310-7-4330.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, StructureSDR 00FDEA00368Skin · crackedDURING ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. FUSELAGE SKIN REPAIR PER FEDEX EO 7-5330-7-2345 PART 2.Jun 5, 2000 · N101FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 00FDEA00367Firewall · crackedDURING ROUTINE INSP NR 2 ENG FIREWALL FOUND CRACKED AT APPROX 8 O''CLOCK POS AT FIRELOOP BRACKET. STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-10-1.Jun 5, 2000 · N101FE · Boeing 72722C · Nacelle/Pylon, Bulkhead/FirewallSDR 00FDEA00366Skin · crackedDURING ROUTINE INSP, FWD LWR CARGO DOOR, EXT SKIN CRACKED IN LWR AFT CORNER. BLENDED OUT CRACK AND INSTALLED EXT DOUBLER IAW SRM 52-00-3.Jun 5, 2000 · N101FE · Boeing 72722C · Cargo/Baggage DoorsSDR RAAA00B2033Battery · dischargedDURING SERVICE CHECK, FOUND PROXIMITY LIGHT INOP AT SEAT ROW 2. REPLACED BATTERY, OPS CHECK GOOD PER RAA ECO 86 - 26. .Jun 4, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA00B2032Battery · dischargedPROXIMITY LIGHT AT ROW 11 WILL NOT TEST. REPLACED BATTERY, OPS CHECK GOOD PER RAA ECO 86-26.Jun 2, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR RAAA00B1067Angle · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION VERTICAL FIN STA 87.00 TRAILING EDGE CHORD LT AND RT SKIN ATTACH ANGLES. CORROSION BEYOND LIMIT. REPAIRED EXTRUDED PARTS IAW SRM 51-40-4, 51-30-2 & 3.Jun 2, 2000 · N831RV · Boeing 72722C · Vertical StabilizerSDR RAAA00B1066Support Bracket · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION UNDER NUT PLATES FWD LOWER SIDE OF SPOILER ACTUATOR SUPPORT. REPAIRED EXTRUDED SECTION IAW SRM 51-40-4 FIG 1.May 31, 2000 · N831RV · Boeing 72722C · SpoilersSDR RAAAOOB1060Stringer · looseDURING SCHEDULED C2 CHECK, FOUND STRINGER REPAIR LOOSE AND WORKING PANEL 9412 STA 110 LT ELEVATOR. REPLACED PREVIOUS REPAIR IAW SRM 55-20-3.May 31, 2000 · N831RV · Boeing 72722C · Elevator, Spar/RibSDR DHL2000706001Fluid · leakingAFTER T/O, TOWER AND ANOTHER A/C REPORTED A SIGNIFICANT AMOUNT OF FLUID LEAKING FROM LFT WING. FUEL WAS DUMPED DOWN TO LANDING WT AND RETURNED TO SERVICE. INSPECTED FUEL LINES AND TANK PANELS, NO LEAKS NOTED. INSPECTED FUEL TANK VENT SYS PER M/M 28-13-00. May 27, 2000 · N706DH · Boeing 72722C · Fuel StorageSDR UPS00232740Floorbeam · corrodedINSPECTION TYPE:C, FLOORBEAM LOWER CHORD CORRODED BS 600 LBL 12 TO 14. CORROSION REMOVED PER SRM 51-10-06, FLOORBEAM REPAIRED IAW SMRO EO 2000-018-006, UPS ENGINEERING FILE NUMBER 727-53-2257.May 26, 2000 · N944UP · Boeing 72722C · Fuselage Main, Floor BeamSDR RAAAOOB2031Battery · dischargedAISLE PROXIMITY LIGHT DOES NOT TEST. REPLACED BATTERY, OPS CHECK GOOD PER RAA ECO NR 86-26.May 26, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR RAAAOOB2030Light · inoperativeEMERGENCY EXIT LIGHT INOP ON P/F. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD PER RAA ECO NR 86-26.May 26, 2000 · N832RV · Boeing 72722C · Emergency LightingSDR UPS00232744Beam · crackedINSPECTION TYPE:C, TAIL SKID COMPARTMENT, TERMINAL-TRANSVERSE BEAM STABILIZING LINK AFT UPPER LT CRACKED. TERMINAL FITTING REPLACED IAW SRM 51-30-2.May 25, 2000 · N944UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS00232737Floorbeam · corrodedINSPECTION TYPE:C&SI, CORROSION UNDER ANCHOR NUT ON CARGO FLOOR, FLOORBEAM AFT CARGO BAY, AT STA 1045 APP AND RBL 8. REPAIR CARRIED OUT IAW SRM 51-30-2 SRM 51-10-6 53-10-5 FIG 4.May 25, 2000 · N944UP · Boeing 72722C · Fuselage Main, Floor BeamSDR RAAA00B1063Skin · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION ON FUSELAGE SKIN, CORROSION BEYOND LIMIT. REMOVED DAMAGED AREA, FABRICATED DOUBLER PER SRM 53-30-3 FIG 1 STEPS 1-10. INSTALLED DOUBLER PER 727 SRM 53-30-3 STEPS 11-15.May 25, 2000 · N831RV · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS00232745Rib · crackedINSPECTION TYPE:C, CRACK FOUND AT I/B RIB NR 5 SLAT. CRACK STOP DRILLED IAW 51-10-01, REPAIR CARRIED OUT IAW SRM 57-50-0 3 FIG 9.May 24, 2000 · N944UP · Boeing 72722C · Leading Edge DevicesSDR RAAA00B1064Skin · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION FUSELAGE SKIN INTERIOR, CORROSION BEYOND LIMIT. REMOVED DAMAGE, FABRICATED DOUBLER PER SRM 53-30-3, INSTALLED DOUBLER PER SRM 53-30-3 STEPS 11-15.May 24, 2000 · N831RV · Boeing 72722C · Fuselage Main, Plate/SkinSDR RAAA00B1062Skin · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION ON VERTICAL FIN SKIN. REPLACED IAW 727 SRM 55-30-3 FIG 1 SHEET 2, 51-20-4, 51-30-2.May 24, 2000 · N831RV · Boeing 72722C · Vertical Stabilizer, Plate/SkinSDR RAAA00B1061Cargo Track · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION ON CARGO TRACK. REPLACED SEAT TRACK BS 1048 RBL13 PER SRM 53-10-5 FIG 8.May 24, 2000 · N831RV · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR RAAA00B1059Skin · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION UNDER FUSELAGE SKIN. REMOVED FASTENERS COMMON TO DAMAGED AREA, REPAIRED IAW 727 SRM 53-30-3 FIG.3M54 960May 24, 2000 · N831RV · Boeing 72722C · Fuselage Main, Plate/SkinSDR RAAA00B1065Stringer · damagedDURING SCHEDULED C2 CHECK, FOUND STRINGER REPAIR DAMAGED. REPAIRED STRINGER IAW SRM 53-10-3 FIG 1 SHEET 4 DETAIL I.May 24, 2000 · N831RV · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS00232742Stringer · corrodedINSPECTION TYPE:C, EVIDENCE OF CORROSION ON STR 18A UPPER AND LOWER FLANGE AT BS 855 RT. CORROSION REMOVED AND REPAIRED IAW SMRO EO 2000-018-004, UPS ENGINE RING FILE NUMBER 727-53-2259.May 23, 2000 · N944UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR RAAA00B1058Web · crackedDURING SCHEDULED C2 CHECK, FOUND WEB CRACKED. REPAIRED IAW 727 SRM 51-40-2, 51-30-2.May 23, 2000 · N831RV · Boeing 72722C · Fuselage Miscellaneous StructureSDR RAAA00B1057Web · crackedDURING SCHEDULED C2 CHECK, FOUND WEB LIGHTENING HOLE CRACKED. STOP DRILLED CRACK AND REPAIRED IAW 727 SRM 51-40-2, 51-30-2.May 23, 2000 · N831RV · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS00232793Skin · dentedINSPECTION TYPE:C, A NUMBER OF SCRATCHES ON FWD CARGO DOOR EXTERNAL SKIN AND DENTS. FWD CARGO DOOR REPLACED IAW MM 52-31-01.May 22, 2000 · N944UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS00232791Drag Link · crackedINSPECTION TYPE:C, EVIDENCE OF CRACK TO TAIL SKID AT TAIL SKID CARTRIDGE ATTACH LUG RT SIDE. TAIL SKID DRAG LINK REPLACED IAW MM 32-71-61.May 22, 2000 · N944UP · Boeing 72722C · Auxiliary Gear (Tail Skid)SDR UPS00232751Skin · dentedINSPECTION TYPE:SI, A NUMBER OF SCRATCHES ON FWD CARGO DOOR EXTERNAL SKIN AND DENTS. DUE TO THE FACT A NUMBER OF THE SHARP CREASES WERE BEYOND SRM LIMITS FWD CARGO WAS REPLACED IAW MM 52-31-01.May 22, 2000 · N944UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS00232734Support Fitting · corrodedINSPECTION TYPE:C&SI, NR 4 FLAP TRACK FWD SUPPORT FITTING UPPER HOLE HAS PITTING CORROSION. REPAIR CARRIED OUT IAW SMRO EO 2000-018-001 UPS ENGINEERING FILE NOL 727-57-2159.May 22, 2000 · N944UP · Boeing 72722C · Trailing Edge Flaps
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