Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 C8GA20050014Fcu · contaminatedFLT 722 FROM TOL TO RDU. IN CRUISE AT FL310, CREW NOTED POWER LOSS OF NR 2 ENGINE ACCOMPANIED BY EPR FLUXUATION, COMPRESSOR STALL, AND VIBRATION. CREW REDUCED POWER SETTING TO IDLE AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO TOL ASDR PCSA0526051Pcu · malfunctionedON TAXI OUT CONTROL YOKE JAMMED WILL NOT MOVE FWD. AC RETURNED TO RAMP. AIRCRAFT WAS FERRIED BACK TO MIAMI. NO DEFECTS REPORTED ON FLIGHT. REMOVED FLOOR PANEL, INSPECTED CONTROL CABLES EBL, EAL, EBR, EAR & PULLEYS BS 540, 740, 870, 950 & 1050 NO DEFECTS. SDR 05FDEA01460Floorbeam · misdrilledUPPER LOBE INTERIOR, STA 520, RBL 43, TOP OF FLOORBEAM HAS DOUBLE DRILLED HOLES. REPAIRED BS 520 UPPER CHORD PER FED-EX EA 7-5310-86321.SDR DHL2005784519Skin · crackedFOUND NR 6 SLAT PREVIOUS REPAIR AT T/E I/B HOOK IS CRACKED. REMOVED PREVIOUS REPAIR AND FABBED NEW IAW 727 SRM 51-30-2 AND 57-50-3 FIG 10 DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 57-50-3 FIG 10.SDR DHL2005784551Doubler · crackedFOUND NR 6 SLAT PREVIOUS REPAIR AT T/E I/B HOOK IS CRACKED. REMOVED PREVIOUS REPAIR. FABBED NEW REPAIR IAW 727 SRM 51-30-2 AND 57-50-3 FIG 10. DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 57-50-3 FIG 10.SDR DHL2005784518Rib · crackedFOUND NR 6 SLAT LE INTERIOR AT WS 491 INBOARD AND OUTBOARD RIBS CRACKED. REMOVED AND REPLACED RIBS AT NR 6 SLAT LE WS 491 INBD AND OUTBOARD IAW B727 SRM 51-30-2 PN 65-17289-20 AND 65-17289-22 BOTH PO NR 5080320.SDR DHL2005784516Tab · delaminatedLT O/B AILERON TAB INB END DELAMINATED (AREA MARKED). REMOVED DELAMINATED EXISTING REPAIR FROM LT O/B AILERON TAB LWR SURFACE, FABRICATED FILLER AND DOUBLER. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES, IAW SDR DHL2005784517Rib · crackedFOUND NR 5 SLAT LE INT AT ACTUATOR ATTACH POINT INBD AND OUT RIBS CRACKED. PREVIOUSLY REPAIRED. REMOVED AND REPLACED DAMAGED RIBS AT NR 5 L/E SLAT ACT ATTACH ON SLAT PN 65-17276U1 AND 65-17276-9 BOTH PO NR 516347 IAW 727 SRM 51-30-2.SDR DHL2005784515Rib · crackedNR 5 SLAT L/E INTERIOR AT ACTUATOR ATTACH POINT INBD AND OUTBD RIBS CRACKED, PREVIOUSLY REPAIRED. REMOVED AND REPLACED DAMAGED RIBS AT NR 5 SLAT L/E SLAT ATTACH ON SLAT P/N 65-17276U11 AND 65-17276-9,BOTH PO NR 518347 IAW B727 SRM 51-30-2.SDR DHL2005784548Web · crackedFOUND VERTICAL STAB SLANT WEB AT 1303 LOWER RIGHT CORNER CRACKED STA 1303, FRAME SECTION ABOVE CENTER INLET DUCT. COMPLIED WITH COTNEY AEROSPACE EA: EAZ04-1 REV : A, 8110-3 DATED 6/8/05. STOP DRILLED CRACK ON VERT STAB WEB BS 1303 RBL 22 IAW 727 SRM 51-10-1 SDR DHL2005784514Frame · dentedSTA 720A FRAME IS DENTED ABOVE STR 23R. FOUND DENT TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1, CUT OUT DAMAGED AREA . FABRICATED ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 3. ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED PART IAW B727 SSDR DHL2005784513Frame · dentedSTA 700 FRAME IS DENTED ABOVE STR 4R. FOUND DENT TO BE OUT OF LIMITS. REPAIRED IAW SRM.SDR 05FDEA01365Frame · damagedFWD CARGO BAY FRAME IS CREASED AT BS 560 STR 24L TO 25L. REPAIRED FRAME PER SRM 51-40-3.SDR 05FDEA01366Skin · crackedCRACK IN SKIN AT BODY STATION 1053 STR 28L.SDR DHL2005783001Connector · dirtyAFTER PLACING LANDING GEAR LEVER FROM UP TO OFF LANDING GEAR DOOR WARNING LIGHT ON FWD PANEL AND RIGHT GEAR DOOR LIGHT ON S OFFICIERS PANEL ILLUMINATED PERFORMED ABNORMAL PROCEDURE. REMOVED CONNECTOR TO RMLG DR SWITCH INSPECTED AND CLEANED CONNECTOR REINSTALSDR DHL2005784512Angle · crackedRT ELEVATOR LOWER SKIN INBD ANGLE SUPPORT AFT OF L/E IS CRACKED AT OUTBD END, ELEV STA 17.2. REPAIRED IAW SRM.SDR DHL2005784511Skin · dentedEMPENNAGE SKIN CREASED BS 1243 AT STR.24R DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. WITH NO DEFECTS NOTED TO STRINGER. REPAIED IAW B727 SRM 51-10-2 AND 53-30-3 FIG 3.SDR DHL2005784510Rib · wornVERT STAB L/E PNL NR 9501 UPPER FORMER RIB IS WORN FIN STA 87. DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-30-1. REPAIRED IAW B727 SRM.SDR DHL2005782002Accessory Unit · malfunctionedWHILE TAXI IN TO STL HEARD ELECTRICAL RELAYS CYCLING OFF AND ON AND THEN SMELLED SMOKE AND A LIGHT HAZE WAS IN THE COCKPIT. AS THE RELAYS WERE CLICKING STALL WARNING AMBER LIGHT FLICKERED OFF AND ON. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT REF MM 32SDR DHL2005784509Frame · bentFWD CARGO FRAME AT BS 680 RIGHT, BENT ABOVE STR 27R TO STR 26R. FOUND DENT TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA, SIZE 1 3/4" BY 1" IAW B727 SRM 53-10-1 FIG 1. FABRICATED ANGLE REPAIR USING 7075-T6 .063 PO 900489, DIM 14 3/16" BY 3 5/8" IAW B727 SRM 53-SDR DHL2005784508Skin · delaminatedNR 7 SPOILER PANEL HAS SMALL DELAMINATION AT INBD TRAILING EDGE CORNER AND TRAILING EDGE PHENOLIC RUB STRIP IS LOOSE AND PEELING OFF, AT WBL 90. REPAIRED.SDR DHL2005784507Skin · gougedLT WING INBD FORE FLAP OUTBD END IS GOUGED BY LONG SCREW, WBL 240. FOUND AREA OUT OF LIMITS. REPAIRED IAW SRM.SDR DHL2005784547Web · crackedVERTICAL STAB SLANT WEB AT 1303 LOWER LEFT CORNER IS CRACKED STA 1303 FRAME SECTION ABOVE CENTER INLET DUCT. COMPLIED WITH COTNEY AEROSPACE EA: EAZ04-1 REV A 8110-3. DATED 6/805 STOP DRILLED CRACK ON VERTICAL STAB WEB BS 1303 LBL 22 IAW 727 SRM 51-10-01 & S/SDR DHL2005784546Bracket · crackedNR 2 LEADING EDGE ACTUATOR UPPER MOUNT IS CRACKED AT LWR INBOARD CORNER, WING STA 224. REMOVED DAMAGED MOUNT ANGLE IAW B727 SRM 51-30-2 AND FABBED NEW FROM 2024T3.063 PO 9002199 DIM 7.375 X 6.5 IAW B727 SRM 57-20-2 FIG 1. TREATED & PRIMED ANGLE IAW B727 SRM SDR DHL2005784506Spar · crackedRT WING NR 7 SLAT SPAR WEB CRACKED AT TAI DUCT CUT OUT AT WS 610.5. STOP DRILL CRACK IAW B727 SRM 51-10-1. NDT IAW B727 NDT MAN 51-00-0. FABRICATED ANGLE USING 2024-T3 .040 PO 9002219. DIM.5 3/4"X 4 1/4" IAW B727 SRM 57-50-3 FIG.4 ALODINE AND PRIME IAW B727SDR DHL2005784505Skin · dentedRT WING, DENT IN NR 6 L/E SLAT AT WS 491 ON L/E. FOUND DENT OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. CUT OUT DAMAGED SKIN IAW B727 SRM 57-50-3 AND INNER SKIN FOR ACCESS. CUT OUT SKIN DIM 10" BY 5" IAW B727 SRM 57-50-3 FIG 1. FAB PART FOR OUTER SKIN REPAIRSDR DHL2005784504Skin · delaminatedLT INBD FORE FLAP IS DELAMINATED ON LOWER SURFACE, WBL 124. REMOVED LT I/B FORE FLAP IAW B727 MM 27-51-00. CUT OUT DELAMINATED AREA AND FABBED FILLER 2 INCH DIA AND DOUBLER AND BONDED REPAIR PARTS IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 3. REINSTALLED LSDR DHL2005784503Tab · delaminatedLT OUTBD AILERON TAB UPPER SURFACE IS DENTED AND LOWER SURFACE IS DELAMINATED AT PREVIOUS REPAIR, WING STA 716. REMOVED DELAMINATED EXISTING REPAIR ON LT, O/B,AILERON TAB LOWER SURFACE CUT OUT APPROX 3 1/4" BY 7 1/2", FABRICATE FILLER APPROX 3 1/4" BY 7 1/2" SDR DHL2005784502Skin · dentedNR 3 SLAT UPPER SKIN IS DENTED AT WING STA.495. EVALUATED AREA TO BE CREASED AND OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. CUT OUT DAMAGED AREA AND FABBED FILLER IAW B727 SRM 57-50-3 FIG 1 REPAIR 4. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 AND ISDR DHL2005784501Mount · crackedNR 1 LEADING EDGE FLAP ACTUATOR UPPER MOUNT IS CRACKED AT LWR OUTBOARD CORNER, WING STA 304. REMOVED UPPER ACTUATOR MOUNT AND FABRICATED NEW ANGLE IAW B727 SRM 57-20-2 FIG 1,TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED NEW ANGLE ON NR 1 LEADING EDGE SDR 05FDEA01280Floorbeam · corrodedUPPER LOBE INTERIOR, STR 950A, LBL 10-22 TOP OF FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM 53-10-8.SDR 05FDEA01279Stringer · crackedFOUND CRACK IN STR 24L BS 560. REPAIRED STRINGER PER SRM 53-10-3.SDR 05FDEA01274Floorbeam · corrodedCORROSION AT FLOORBEAM FASTENER HOLES BS 720 RBL 50 LBL 50, WL 200. REPAIRED FLOORBEAM PER SRM 53-10-8.SDR 05FDEA01278Skin · dentedDENT IN SKIN BS 1348, STR 22L. REPLACED SKIN PANEL PER SRM 51-30-2.SDR 05FDEA01277Skin · dentedDENT IN SKIN BS 1347, STR 7L. REPLACED SKIN PANEL PER SRM 51-30-2.SDR 05FDEA01276Skin · dentedDENT IN SKIN AT BS 1348, STR 14L. REPLACED SKIN PANEL PER SRM 51-30-2.SDR 05FDEA01272Power Unit · leakingDURING FLAP RETRACTION INDICATORS SHOWED SPLIT FLAP W/INBOARDS REMAINING AT 2 DEG W/FLAP UP. AFTER RUNNING QRH AND INBOARDS GOING TO FULL UP, HYD A SYSTEM INDICATED 0 QTY. RAN QRH AGAIN W/ALTERNATE FLAPS SYSTEM AND MANUAL GEAR EXTENSION PROCEDURES. WHEN ASDR XN0A1236Warning Light · illuminatedDURING EMERGENCY DESCENT, LT DUCT OVERHEAT LIGHT TRIP, PERFORMED ALL CHECKLIST.SDR XN0A1235Ignition Unit · malfunctionedNR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD.SDR XNOA1225Engine · inoperativeNR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD.SDR 05FDEA01143Cylinder · damagedWITH FLAPS SET AT 15 DEG, WHEN LANDING GEAR PLACED FROM OFF TO DOWN, A SYS HYD PRESSURE WENT TO ZERO, A HYD QUANTITY WENT TO ZERO. RAN QRH PROCEDURES. LEFT AND RIGHT MAINS WERE GREEN, NOSE GEAR INDICATING UP PRIOR TO RUNNING CHECKLIST. MANUALLY EXTENDED GESDR 05FDEA01114Angle · damagedWHILE CLOSING AFT CARGO BAY THRESHOLD FOUND LOWER ANGLE AT BS 990 TO BE DAMAGED. REPAIRED DAMAGED AFT CARGO BAY THRESHOLD LOWER ANGLE BS 990 PER FED EX EA 7- 5310-86283.SDR XN0A1232Warning Light · illuminatedALL THREE LIGHTS ILLUMINATED ON NR 1 GENERATOR. TRANSFERRED TO DMI 5350 IAW ENA MEL 24-1. PLACARDS INSTALLED, SP COMPLIED WITH.SDR 05FDEA01055Fitting · corrodedVERTICAL FIN TENSION TIE RIB LEFT AFT VERT BOLT HOLE CORRODED A/C AND TENSION TIE SIDE. REPAIRED VERT FIN TENSION TIE RIB LT AFT VERT BOLT HOLE PER FED EX EA 7-5530-86280SDR 05FDEA01056Fitting · corrodedCORROSION VERT STAB TENSION TIE AFT SHEER FITTING UPPER SURFACE. REPAIRED VERTICAL FIN TENSION TIE AFT SHEAR FITTING PER FED EX EA. 7-5530-86280.SDR DHL2005783514Skin · damagedLT FUSELAGE SKIN HAS 2EA CREASES AFT OF BS 1130 ABOVE STR 26L (BELOW PREV REPAIR). REMOVED PREV REPAIR BS 1130 ABOVE STR26L IAW B727 SRM 51-30-2, DAMAGED FOUND TO OUT OF LIMITS IAW B727 SRM. REPAIRED IAW SRM.SDR 05FDEA01047Switch · out of adjustMAIN CARGO DOOR B LIGHT CAME ON AT 16,000 FT, DURING CLIMB. FLAPS WERE RETRACTED ALREADY. NO LOSS OF PRESSURIZATION. LIGHT WENT OUT AT 7000 FT DID NOT COME BACK ON. FOUND MAIN CARGO DOOR 'B' SWITCH OUT OF ADJUSTMENT ('A' DOOR LIGHT CAME ON BEFORE 'B' LSDR 05FDEA01045Shear Tie · tool damageVERTICLE STAB TENSION TIE FWD SHEAR TIE FITTING HAS PREVIOUS TOOLING MARKS. REPAIRED PER EA 7-5530-86281.SDR DHL2005783511Skin · dentedFUSELAGE SKIN DENTED BS 1070 ABOVE STR 23 RT. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS AT STA 1070 STR 23R IAW SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1.75 BY 3.75 AND FABRICATED DOUBLER REPAIR FROM MAT USED 2024T3 .071 PSDR DHL2005783510Skin · misrepairedACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON NR 2 SLAT AT WS600 PER ASTAR JC FCD500001-018-B. PREVIOUS REPAIR FOUND TO BE NON-COMPLAINT IAW 727 SRM 57-50-3 FIG 1. FABRICATED DOUBLER USING 2024T3 .080 PO NR 9002012 DIM. 9 1/2" BY 7 3/4" IAW B727 SRM 57-50-
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