Boeing 727-200
Service difficulty reports · 2,835
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 = '727200' 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 = '727200' 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 FDEA200905121929Skin · crackedNR 3 ENGINE NOSE COWL EXTERIOR SKIN CRACKED AND CHAFED AT T/E, APPX 4 O'CLOCK. CUT-OUT DAMAGE AREA IAW SRM 51-10-1 AND FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 5SDR FDEA200905121928Skin · crackedNR 1 ENGINE NOSE COWL AFT EXTERIOR SKIN OTBD SIDE AT 9 O'CLOCK POSITION. AFT T/E SKIN EDGE IS BENT OUT AND CRACKED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR AND FILLER AND INSTALLED REPAIR IAW SRM 54-30-3, 51-30-2, 51-10-1 AND 51-10-2.SDR C8GA20090064Fan · bentFLT 706 FROM ILN TO MSP, DURING TAKEOFF ROLL THE NR 3 ENGINE HAD A COMPRESSOR STALL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 ENGINE HAD INGESTED A GOOSE. THE C1 AND C2 FSDR C8GA20090054Indicator · failedFLT 1735 FROM QRO TO GDL. DURING TAKEOFF ROLL THE CAPITAL'S AIRSPEED INDICATOR FAILED TO INDICATE AIRSPEED. THE TAKEOFF WAS ABORTED. POST FLIGHT INSPECTION WAS PERFORMED FOUND CAPTAIN'S AIRSPEED INDICATOR TO BE AT FAULT. AIRSPEED INDICATOR WAS REMOVED AND RSDR I5PA0308091Actuator · defectiveAIRCRAFT, AIR RETURN DUE TO NR 3 L/E SLAT REMAINED EXTENDED AND NR 3 SLAT REMAINED IN TRANSIT DURING FLAP RETRACTION. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR THEN CLEANED AND RESEATED NR 2 L/E SLAT SWITCH. OPERATIONAL CHECK OK.SDR I5PA030809Transceiver · malfunctionedAIRCRAFT, AIR RETURNED DUE TO NR 1 AND NR 2 HF'S WOULD NOT TRANSMIT OR RECEIVE. CLEANED AND RESEATED BOTH TRANSCEIVERS, OPS CHECK WITH SFO NORMAL. OK FOR SERVICE NO FURTHER PROBLEMSSDR FDEA200901050041Spar · crackedRT WING T/E, FALSE SPAR INBD ATTACHMENT HAS LOOSE HARDWARE AND SEPARATION BETWEEN PARTS, WBL 118 FOUND CRACKED. REPAIR ACCOMPLISHED PER DRAWING SR27-57-038 REV "C". STD. REWORK DRAWING INBD BEAM CRACK REPAIR.SDR DHLA2008743519Flap Track · corrodedREF N/R 5-222, LT WING NR3 T/E FLAP TACK AFT AND FWD SURFACES WITH CORROSION. REPAIRED LT WING NR 3 T/E FLAP TRACK AFT AND FWD MOUNTING PADS IAW OHM 57-40-01 PAR 2 B PAGE 403 AND PARA 2.E PAGE 411.SDR 2008FA0000746Pump · malfunctionedCRUISE NR 1 ENG STARTED TO SPOOL DOWN OTHER PARAMETERS ARE NORMAL, PERFORMED IN-FLIGHT START CHECKLIST SEVERAL TIMES INCLUDING RESETTING SWITCHES, NO LIGHT OFF. ACFT DIVERTED AND THE CREW PERFORMED ENG INSPECTION AND START ON NR 1 ENG HIGH IGNITION SYS, ENGINESDR DHL2008F00045Light · inoperativeCOCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-93. OP CHECK GOOD. ACFT GROUNDED. (K)SDR C8GA20080039Skin · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSP. FOR DTA FOUND EXISTING EXTERNAL FUSELAGE REPAIR AT STA. 684 STR. 27R TO BE NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR,CUT OUT DAMAGE AND VERIFIED CRACK CONTAINMENT. FABRICATED FILLER AND FABRICATED DOUBLESDR C8GA20080038Skin · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSP. FOR DTA FOUND EXISTING EXTERNAL FUSELAGE REPAIR AT STA. 684 STR. 27L TO BE NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR,CUT OUT DAMAGE AND VERIFIED CRACK CONTAINMENT. FABRICATED FILLER AND FABRICATED DOUBLSDR 08FDEA03522Pump · malfunctionedAT FL 350 IN STEADY CRUISE FLT, FELT SLIGHT VIBRATION FOLLOWED BY NR 1 EPR ROLL BACK, NR 1 N1,N2 EGT ROLLBACK. N1 STABILIZED AT 26 PERCENT, EGT 180 DEG NR 1 GEN BREAKER LIGHT ON AND NR 1 LOW OIL PRESSURE LIGHT ON. THRUST LEVEL BOUGHT TO IDLE AND DESCENT STARSDR DHLA200800080Transmitter · malfunctionedFLT 577, DURING ENG ACCELERATION NR 3 EPR FLUCTUATES RAPIDLY. ALL OTHER ENG PARAMETERS NORMAL. BRAKE ENERGY NORMAL. DEFERRED PER MEL 77-1-1, DMI CONTROL 3319. MAINTENANCE CONTROLLER RPR AT 0942(Z). AIRCRAFT GROUNDED. REMOVED AND REPLACED NR 3 ENG EPR TRASDR 08FDEA02949Web · crackedRIGHT WING O.B. L.E. NR 5 SLAT BN 279, CRACKED LWR. AFT INTERNAL WEB ANGLE AT INBD. SIDE OF ACTUATOR RAM ATACH STRUCTURE REMOVED ACCESS PANEL, INSPECTED FOR CRACKS, VERIFIED MATERIAL, FABRICATED, LOCATED AND DRILLED REPAIR PART. INSTALLED REPAIR, INSTALLED ACSDR 08FDEA02839Stringer · crackedRT WING, STR 10, CRACKED AT W.S. 686.5, ITEM IS AD DRIVEN, IF CRACKS EXCEED LIMITS IN SECTION II, FIG 12, CONTACT STRUCTURES ENGINEERING FOR REPAIR INSTRUCTIONS PER WORK CARD E7-5710-7-4322. STOP DRILLED CRACK. NDT TO VERIFY TERMINATION OF CRACK AT STOP DRILSDR 08FDEA02827Frame · damagedINTERIOR FUSELAGE STA 344 STRINGER TIE AT STR 7R HAS 02 FASTENERS WITH "O" ED. REMOVED STRINGER TIE IAW B727 SRM 51-30-2, CUT OUT DAMAGE FRAME DIM 1.5 X 5/8 IAW B727 SRM 53-10-4 FIG 2. FABRICATED NEW STRINGER TIE FROM 7075T6 .032 DIM 3 X 3.75. FRAME REPAIR SDR 08FDEA02759Skin · gougedDEEP GOUGE IN LT O/B FOREFLAP, L/E CAP UPPER SURFACE APPROX 10 INCHES FROM I/B END IN PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1' X 5/8 IAW B727 SRM 57-50-4 FIG 1. FABRICATED REPAIR PLATE MAT USED 2024T3 .063' SDR 08FDEA02513Valve · failedCABIN PRESSURE WOULD NOT HOLD WITH ACFT AT 240. DESCENT TO 200 HELPED FOR ABOUT 1 HOUR, THEN CABIN CREAPED UP TO 9500'. FURTHER DESCENT TO 18000 ALLOWED CABIN TO HOLD STEADY. MAINTENANCE ACTIONS, REPLACED RT PACK VALVE.SDR C8GA20080019Sensor · inoperativeFLT 245 FROM EWR TO BDA. DURING TAKEOFF THE NR 2 ENG HAD A HIGH OIL TEMP LIGHT, CREW PERFORMED ENG SHUTDOWN AND THE ACFT RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 2 ENG OIL TEMP BULB WAS AT FAULT. REMOVED SDR C8G2008F00005Bulb · inoperativeDURING TAKEOFF THE NR 2 ENG HAD A HIGH OIL TEMP LIGHT, CREW PERFORMED ENG SHUTDOWN AND THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 2 ENG OIL TEMP BULB WAS AT FAULT. REMOVED AND REPLACED OIL TEMP SDR DHLA200800051Light · inoperativeFLT 119 - DURING PREFLIGHT STBY POWER CHECK, L1 EXIT DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. CLEANED & RESEATED EMERGENCY FWD ENTRY LIGHT ASSY & PERF OPS CK IAW AOM 1.3, PG 7, SYS OPS CHECK GOOD. AIRCRAFT WAS GROUNDED.SDR DHLA200800050Actuator · leakingFLIGHT 1612 ON TAKEOFF ROLL, A/C SUSTAINED HYD A-SYSTEM FAILURE PRIOR TO 60 KIAS. FOUND NR 5 KRUEGER FLAP LEAKING. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR. SERVICED A-SYS. INSP NR 1 & 2 CASE DRAIN FILTERS. OPS CHECK GOOD. NO FURTHER LEAKS NOTED. SDR G8G2008F00000Accessory Unit · malfunctionedDURING CRUISE OPERATION CAPTAIN’S RMI CARD AND FO`S HSI CARD STOPPED TURNING IN FLIGHT, BOTH RMI NEEDLES FROZE IN POSITION. AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THE FLIGHT INSTRUMENT ACCY UNIT AT FAULT. RESDR 08FDEA01941Doubler · crackedNR 3 ENG LOWER COWL, I/B SIDE EDGE, 3RD LATCH CUTOUT FROM FWD END, LOWER CUTOUT AREA, DOUBLER CRACKED OUT. REMOVED AND REPLACED DOUBLER, REF SRM 51-30-2 PG 2, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01940Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM / DISBONDED. COMPOSITE REPAIR, BS 1176 - 1183, RBL 27-37, WL 208. REMOVED CRACKED DITCHING PAN. FABRICATED NEW DITCHING PAN, HEAT TREATED TO T-6 CONDITION, TREATED AND PRIMED, AND INSTALLED. REFSDR 08FDEA01939Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176-1183, RBL 37-47 WL 208 (MKD). FABRICATED NEW DITCHING PAN, HEAT TREATED, ALODINED AND PRIMED, INSTALLED IAW SRM 51-10-2, PG 1, 51-30-2, PG 1, 51-30-5 PG 1. BOEING DWD: 65SDR 08FDEA01857Hose · chafedCRUISING AT 380, OIL QUANITY DECREASED FROM 3 QUARTS TO JUST OVER 1 QUART. PRESSURE RANGED FROM 41-38 PSI. INSTALLED TEMP FLEX LINE IAW EA 7-7930-121858. LEAK CHECK GOOD. SERVICED OIL AS REQUIRED. REQUIRES TUBE MFG 259-1112-504 TO FINALIZE THE REPAIR BSDR 08FDEA01838Indicator · failedCAPT'S AIRSPEED INDICATOR NOT WORKING. NO AIRSPEED INDICATION- AIARSPEED FLAG IN VIEW. REMOVED AND REPLACED CAPT'S AIRSPEED IND PER MM 34-12-021-4. AC OK TO CONTINUE.SDR 08FDEA01712Angle · crackedRIB NR 2 ATTACH ANGLE CRACKED AT STR 6R ATTACHMENT BOLT INSIDE VERTICAL STAB, STR 6R, RIB NR 2 FIN STA 22.5 CUT-OUT DAMAGED AREA IAW SRM 51-10-1 & 55-30-5 FIGURE 1, FABRICATED REPAIR ANGLE & REPAIR FILLER, TREATED & PRIMED PARTS IAW SRM 51-1-2, INSTALLED REPSDR 08FDEA01486Fairing · crackedRT WING NR 6 FLAP TRACK FWD FAIRING HAS SEVERAL CRACKS REMOVED FASTENERS AND FABRICATED NEW REPAIR DOUBLER. INSTALLED NEW DOUBLER REF SRM 57-20-4 FIG 1. TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 P2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR DHLA200800039Trim Switch · brokenFLT 589, WHEN THRUST LEVERS ADVANCED FOR TAKEOFF, TAKEOFF WARNING HORN ACTIVATED. FLAPS 15 SPEED BRAKES STOWED TRIM SET AT 6.6. FOUND UPPER STAB. TRIM SWITCH (S532) RETURN MECHANISM BROKEN. R&R SWITCH IAW MM 31-26-24 & WDM 27-43-01. TESTED TAKE-OFF WARNING ISDR 08FDEA01306Floorbeam · corrodedMAIN CARGO COMP STA 760-848 LBL 24 T-CAP CORRODED REMOVED SEAT TRACK AND T-CAP IAW SRM 51-30-2. LOCATED AND DRLLED NEW T-CAP IAW SRM 53-10-2 FIG 7 AND 51-30-5. TREATED AND PRIMED NEW T-CAP IAW SRM 51-10-2. INSTALLED NEW T-CAP AND SEAT TRACK AT MAIN CARGOSDR CA080328011Duct · leaking(CAN) AFTER TAKEOFF OUT, NR 2 ENGINE FIRE WARNING CAME ON. THE THROTTLES WERE RETARDED AND THE WARNING EXTINGUISHED. THE AC RETURNED TO AIRPORT. AFTER INVESTIGATION, MAINTENANCE FOUND THE DUCT FOR THE FUEL HEAT VALVE HAD COME OUT OF ITS SLEEVE CAUSING A DUCT SDR 08FDEA00645Circuit Breaker · failedWITH ENGINE NR 2 RUNNING, SMOKE ENTERED COCKPIT FROM UNKNOWN SOURCE. GOT INTERMITTENT NR 3 MAIN CARGO BAY SMOKE ALARM & LIGHT. ALARM & LIGHT OCCURED 2 TIMES FOR 1 SEC. SHUTDOWN NR 2 ENGINE & POWERED ACFT WITH APU. SMOKE DISPERSED. ON APU & EXT POWER, NR 2 BUSSDR 08FDEA00412Seat Track · corrodedMAIN CARGO COMPARTMENT, SEAT TRACK CORRODED IN NUMEROUS PLACES FROM BS 360-400, LBL 24. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-2 FIG7 AND 53-10-1 FIG3, SRM PAGE 23. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACKSDR 08FDEA00411Skin · damagedAFT CARGO COMPARTMENT FRAME SHEAR TIE HAS IMPROPER RIVET INSTALLATION ON FWD SIDE. RIVET INSTALLED THRU ANOTHER RIVET AT STA. 970, STR 25-26L. REMOVED RIVETS FROM SHEAR TIE AND FAIRING ATTACHMENT SUPPORT IAW SRM 51-30-2. CUT-OUT DAMAGED SKIN. FABRICATED REPAISDR DHL2008749015Nose Cowl · dentedDURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE COWL TO COWL LIP FLANGE IS BENT, DENTED, AND METAL PIECE BROKEN OFF. CUT OUT DAMAGE AREA ON NR 1 ENGINE NOSE COWL AFT TRAILING EDGE DIMENSION CUT OUT 1.75 INCH BY .5 INCH IASDR 08FDEA00170Web · crackedLT WING , RIB ATTACH FTG FOR O/B AILERON AT NR 2 HINGE I/B AND O/B WEBS BROKEN OUT HINGE ATTACH BOLT. REMOVED O/B HINGE WEB NR 2 O/B, FABRICATED, TREATED AND PRIMED AND INSTALLED NEW WEB REF SRM 51-30-2 PG 4-5. BAC DOC 65-19275, BAC DWG 65-19260 REV G, THIS SDR 08FDEA00169Seat Track · corrodedFWD CABIN, RIGHT O/B SEAT TRACK, UPPER SURFACE HAS LIGHT CORROSION AS MARKED FROM STATION 420 -440, RBL 46" WL 208 REMOVED CORROSION BS 420 - 440, RBL 46, WL 208, ORIGINAL THICKNESS .070", .063 REMAINING .007 MAT LOSS. OUT OF LIMITS REF SRM 51-10-1, BAC 1520-SDR 08FDEA00014Cylinder · leakingON CLIMBOUT, "MCD ARM" LIGHT AND "CARGO DOOR IN-TRANSIT" LIGHT ILLUMINATED, REPEAT WRITE UP.PRESSURIZATION WAS NORMAL THROUGHOUT FLIGHT. AT TIME OF LIGHT ILLUMINATION, PSID WAS 6. APPX ALTITUDE WAS 15,000. R & R MCD AFT LATCH CYLINDER PER 52-34-021-4. BLESDR 07FDEA04996Blocker Door · out of adjustMAIN CARGO DOOR "A" OPEN LIGHT ILLUMINATED INFLIGHT, PRESSURIZATION NORMAL INITIALLY, FLICKERED AT FL 200 THEN REMAINED ON STEADY IN DESCENT UNTIL SHORT FINAL THEN WENT OUT. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXPIRATION: 14DEC07 "MELSDR 07FDEA04761Stringer · corrodedAFT PIT STR 28L HAS CORROSION BET STA 1053 TO STA 1054 CORROSION FOUND DURING REPAIR ON N00489 AFTER SKIN WAS REMOVED CUT OUT DAMAGED STRINGER. FABRICATED REPAIR PARTS TREATED AND FR PRIMED. INSTALLED STRINGER REPAIR REF SRM 53-10-3 FIG 1. THIS REPAIR IS CLSDR 2007FA0000946Stringer · crackedTHE AIRCRAFT INPUT FOR 4C CHECK AND CPCP ON SEPT 3, 2007. DURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND 5 INCH CRACK BOTH ON LT AND RT FUSELAGE STRINGER S18A BETWEEN BS940 AND BS945 ON SEPT 21, 2007. A PROPOSAL WAS INITIALLY SUBMITTED ON SSDR 07FDEA02223Display · burnedPDIS 465 26-12 0009505 20JUN07 PIT OPEN R LOGPAGES: 01339908 APPROX 1 00 HOURS INTO FLIGHT, ALL CREWMEMBERS SMELLED A BURING SMELL AND SAW LIGHT SMOKE, SOURCE UNKNOW. PREFORMED PHASE ONES RED TAB PROCEDURE. DIVERTED INTO KPIT ENT BY: 001395 RPSDR 07FDEA02041Seat Track · corrodedCABIN FLOOR SEAT TRACK HAS CORR, FS 460-620, RBL-24". REMOVED CORRODED SEAT TRACK AT RBL 24 , STA 480 TO 620 IAW B727 SRM 53-10-5. FAB NEW SECTION OF SEAT TRACK PO 1142187. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-SDR 07FDEA01988Attach Fitting · crackedMAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 351 FWD, STR 15L. REMOVED WEB, REMOVED CLIP, DRILLED AND INSTALLED NEW CLIP, REINSTALLED WEB REF SRM 51-30-2 FIG.SDR 07FDEA01705Stop Fitting · crackedMAIN DECK RT AFT OVER WING DOOR CUTOUT HAS 1 EA STOP PAD CRACKED AT FWD UPP POS BS 825 REMOVED AND REPLACED STOP PAD REF. 52-20-002-8 PG.1SDR 07FDEA01704Stop Fitting · crackedMAIN DECK RT RWD OVER WING DOOR CUTOUT HAS 4 EA CRACKED STOP PADS AT THE FOLLOWING POS: FWD UPP, AFT UPP, AFT MID, LWR BS 760-783. REMOVED AND REPLACED STOP PADS (4 EA) REF MM 52-20-002-8 PG1.SDR 2007FA0000588Brake Disc · malfunctioned(REG NR: HP1610) DURING PREFLIGHT INSPECTION, FOUND MAIN TIRE NR 2 WITH FLAT SPOT. ON THIS AIRCRAFT OP SPECS APPROVED BY THIS DGAC, OPERATING BY DHL OF GUATEMALA UNDER THEM. REMOVED AND REPLACED MWA AND BRAKE ASSY. NR 2 DUEL TO DAMAGED , ALSO MAIN WHEEL AS
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