Boeing 727-228
Service difficulty reports · 1,323
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 = '727228' 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 = '727228' 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 DHL200072107CPanel · delaminatedRT WING RT UPPER SURFACE O/B OF SPOILER NR 14, PANEL 8855 HAS DELAMINATION. REMOVED PANEL PER SRM 51-30-2. INSTALLED COMPOSITE REPAIR PER SRM 51-40-6. REINSTALLED PANEL PER SRM 51-30-2.SDR DHL20007210Panel · delaminatedRT WING RT UPPER SURFACE O/B OF SPOILER NR 14, PANEL 8855 HAS DELAMINATION. REMOVED PANEL PER SRM 51-30-2. INSTALLED COMPOSITE REPAIR PER SRM 51-40-6. REINSTALLED PANEL PER SRM 51-30-2.SDR DHL200072106Panel · delaminatedRT WING RT UPPER SURFACE O/B OF SPOILER NR 14, PANEL 8855 HAS DELAMINATION. REMOVED PANEL PER SRM 51-30-2. INSTALLED COMPOSITE REPAIR PER SRM 51-40-6. REINSTALLED PANEL PER SRM 51-30-2.SDR DHL200072106CSkin · delaminatedRT WING RT UPPER SURFACE O/B OF SPOILER NR 14, PANEL 8855 HAS DELAMINATION. REMOVED PANEL PER SRM 51-30-2. INSTALLED COMPOSITE REPAIR PER SRM 51-40-6. REINSTALLED PANEL PER SRM 51-30-2.SDR DHL200072102CWeb · crackedMAIN CARGO DOOR HAS INTERNAL HORIZONTAL WEB CRACKED AT BS 650 STR 13 LEFT. PARTIAL REMOVE INNER SKIN AS PER SRM 51-30-2. REMOVED CRACKED HORIZONTAL WEB AS PER SRM 51-30-2. REPLACED WEB AS PER SRM 51-30-2. INSTALLED PARTIAL INNER SKIN AS PER SRM 51-30-02.SDR DHL2000726004Valve · not closedREJECTED TAKEOFF FOR LOW EPR NR 1 ENGINE. FOUND NR 1 ENG ANTI ICE VALVE IN WRONG POSITION. MOVED NR 1 ENG ANTI ICE VALVE TO CLOSED POSITION WITH SWITCH. NORMAL TAKEOFF.SDR DHL200072145CPanel · delaminatedRIGHT WING LOWER SURFACE PANEL NR 8506 HAS DELAMINATION AT O/B OF NR 6 FLAP TRACK. REMOVED PANEL PER SRM 51-30-2 AND ROUTED TO F/G SHOP FOR REPAIR. INSTALLED COMPOSITE REPAIR PER SRM 51-40-6. REINSTALLED PANEL PER SRM 51-30-2.SDR DHL200072143CStructure · damagedLEFT HORIZ STAB TIP UPPER SURFACE DAMAGED. REMOVED LT HORIZ STAB TIP AND ROUTED TO F/G SHOP PER SRM 51-30-2. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8. REINSTALLED TIP ON STAB PER SRM 51-30-2.SDR DHL200072141CStructure · crackedAIRSTAIR AREA RT SECTION APPROX BS 1335 STRINGER 17 IS CRACKED AT ATTACH POINT TO ANGLE SUPPORT. CUT AND REMOVED 9 INCH SECTION OF STRINGER 17R FROM BS 1329 TO BS 1338 PER SRM 53-10-3. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-10-3. TREATED AND PRIMED PSDR DHL200072104CSpar · crackedRIGHT WING L/E CAVITY WS 130.7 LATERAL WEB UPPER CHORD CRACKED AT DIFFERENT PLACES (5 EA). CRACKS RUNNING FROM ATTACHING BOLTS. REMOVED FASTENERS ON CRACKED ANGLE PER SRM 51-30-2. CUT OUT DAMAGED AREA, FABRICATED FILLER ANGLE PER SRM 51-40-4. INSTALLED REPSDR DHL200072146CCowling · damagedNR 1 INLET COWL AFT O/B FLANGE DAMAGED ABOVE AND BELOW O/B HORZ LATCH 8 TO 10 O''CLOCK. CUT OUT DAMAGED AREA AND REMOVED FASTENERS, FABRICATED ANGLES PER SRM 54-10-3. INSTALLED ANGLES PER SRM 54-10-3. TREATED AND PRIMED PER SRM 51-10-2. CLOSED ALL ACCESS PSDR DHL200072105CPanel · delaminatedRIGHT WING AT I/B OF NR 6 FLAP TRACK, REAR SPAR AREA, PANEL NR 8505 HAS DELAMINATION. REMOVED PANEL 8505 PER SRM 51-30-2 AND ROUTED TO FIBERGLASS SHOP FOR REPAIR. INSTALLED COMPOSITE BOND REPAIR TO PANEL PER SRM 51-40-6. INSTALLED PANEL PER SRM 51-30-2.SDR DHL200072147CSpar · crackedRIGHT WING L/E CAVITY FRONT SPAR UPPER CHORD WS 735.5 SHOWS CRACK ABOUT 8 INCHES LONG JUST ABOVE NR 8 SLAT HYD ACTUATOR SUPPORT. REMOVED FASTENERS PER SRM 51-30-2. REMOVED STIFFENER TO GAIN ACCESS PER SRM 51-30-2. TRIMMED AREA OF CRACK PER SRM 57-10-6. HFESDR DHL200072101CFloor Panel · brokenFWD CARGO COMPT FLOOR PANEL 3.5 X 3.5 REPAIR HAS BROKEN AND SHARP EDGES AT FS 660. REMOVED EXISTING REPAIR PER SRM 57-30-2. CUT OUT DAMAGED FLOOR PANEL 4 X 4.5 INCH AND INSTALLED FLUSH DOUBLER REPAIR PER SRM 51-40-2.SDR DHL2000724002Engine · malfunctionedAFTER BEING CLEARED FOR T/O (A) KIAH, AIRCRAFT WAS TAXIED INTO POSITION AND POWER ADVANCED FOR T/O, NO EPR INDICATION ON NR 2 ENGINE. TAKEOFF WAS REJECTED BELOW 5 KTS. THIS WAS TRANSFERRED TO DMI LOG ON MEL 77-1 REF CNTL NR 1758.SDR DHL200072140CPanel · delaminatedRT WING TOP PANEL JUST AFT OF APU EXHAUST DELAMINATED. REMOVED APU EXHAUST DUCT PER M/M 49-80-0. REMOVED APU EXHAUST PANEL PER SRM 51-30-2 AND ROUTED TO F/G SHOP FOR REPAIR. INSTALLED REPAIR TO PANEL PER SRM 51-40-6. INSTALLED PANEL PER SRM 51-20-4. REINSSDR DHL2000726003Switch · out of adjMAIN CARGO DOOR UNLOCK LIGHT ILLUMINATED AFTER T/O AT 6000 FT. DEPRESSURIZED CABIN, LIGHT EXTINGUISHED. ADJUSTED MAIN CARGO DOOR WARNING SWITCHES PER M/M 52-7-0.SDR DHL2000721004Engine · malfunctionedDURING T/O AFTER V2 NR 3 ENG EGT CAME UP TO 620 DEGREES FOR 25 - 30 SECONDS. ABNORMAL PROCEDURE COMPLETED INCLUDING INFLIGHT ENG SHUTDOWN. RETURNED TO IAH.SDR DHL2000721003Engine · malfunctionedDURING TAKEOFF (APPROX 100 KTS) NR 3 ENG WOULD NOT MAKE T/O TRUST AT 1.94 MAX EPR WITH T/L FULL FWD WAS 1.90 WITH PACKS ON. INSP ENG INLET & EXHAUST, NO DEFECT NOTED. DRAINED MOISTER TRAP. TRIMMED NR 3 ENG PER JRH 07-01, ALL PARAMETERS CK WITHIN LIMITS.SDR DHL200072121CPanel · delaminatedRT WING (TOP) PANEL JUST AFT OF APU EXHAUST DELAMINATED. INTERIM REPAIR INSTALLED PER AERONAUTICAL SOLUTIONS 00-0051R. COMPLETE PREM REPAIR. REMOVED APU EXHAUST DUCT PER M/M 49-80-0. REMOVED PANEL PER SRM 51-30-2 AND ROUTED TO F/G SHOP FOR REPAIR. INSTALLSDR DHL200072120CPanel · delaminatedRT WING (TOP) PANEL JUST AFT OF APU EXHAUST DELAMINATED. INTERIM REPAIR INSTALLED PER AERONAUTICAL SOLUTIONS 00-0051R. COMPLETE PREM REPAIR. REMOVED APU EXHAUST DUCT PER M/M 49-80-0. REMOVED PANEL PER SRM 51-30-2 AND ROUTED TO F/G SHOP FOR REPAIR. INSTALLSDR DHL200072112CPanel · delaminatedRT WING (TOP) PANEL JUST AFT OF APU EXHAUST DELAMINATED. INTERIM REPAIR INSTALLED PER AERONAUTICAL SOLUTIONS 00-0051R. COMPLETE PREM REPAIR. REMOVED APU EXHAUST DUCT PER M/M 49-80-0. REMOVED PANEL PER SRM 51-30-2 AND ROUTED TO F/G SHOP FOR REPAIR. INSTALLSDR DHL2000724001Gyro · intermittentADI ATTITUDE FLAG ON CAPT SIDE APPEARS INTERMITTENTLY. REMOVED AND REPLACED NR 1 VERTICAL GYRO PER M/M 34-22-21. OPS CHECK NORMAL.SDR DHLA200062301Door · openTHE 1P AC FAILED TO PRESSURIZE AFTER T/O IN AUTO, STBY, AND NORMAL MODE. THE 2P FWD ENTRY DOOR FAILED TO OPEN AFTER BLOCK IN. THE 1P PRESSURIZED AC, SYSTEM OPS CHECK NORMAL IAW 21-30-0. THE 2P FOUND FWD ENTRY DOOR IMPROPERLY CLOSED. OPENED AND CLOSED DOOR,SDR DHL2000720002Fcu · malfunctionedNR 1 ENGINE IDLE LOW 48 PERCENT N2 28.5 PERCENT N1 AFTER 12 SECONDS NR 1 ENG WAS NOT AT 1.6 EPR DID NOT MAKE T/O POWER AT 40 KTS/RTO. REPLACED NR 1 ENG FUEL CONTROL UNIT PER M/M 73-21-2. PERFORMED ENG POWER TEST PER JRH 06-04-02, ALL PARAMETERS CHK WITHIN LISDR DHL2000726002Engine · failedNR 1 ENGINE FAILED AFTER TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE. LEAK AND OPS CHECKED OK PER B727 M/M 71-00.SDR DHL200072101Line · crackedPER ITEM 1-P,NR 3 EGT REACHED REDUCED JUST AFTER V-1,T/L 3 AHEAD OF 1 & 2. NR 3 REDUCED TO 1.60 EPR GIVING APPROX 85 PERCENT N1 & 90 PERCENT N2. EGT WAS AT TOP OF YELLOW. FUEL FLOW APPEARED NORMAL. FOUND PS-4 LINE TO PRBC CRACKED. REPLACED LINE, GROUND RASDR DHL200072001Socket · failedNR 1 ENGINE OIL TEMP INDR FLUCUATING. REMOVED AND REPLACED NR 1 ENG OIL TEMP BULB SOCKET.SDR DHL200072618CStrap · corrodedFWD BAG BIN HAS CORROSION AT STA 700 RBL 45 ON GILL LINER ATTACH STRAP. REMOVED CORROSION PER SRM 51-10-6, ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072630CSkin · dentedDENT AT BS 520 AT STR 23R ON EXT SKIN INTERM REP, IN PLACE, REPAIR AT NEXT C-CHECK. REMOVED FASTENERS PER SRM 53-30-3. REMOVED OLD DOUBLER PER SRM 51-30-2. REMOVED PITOT STATIC PORTS AND LINES PER M/M 34-10-00. DYE PENETRANT INSPECTION PER NDT MAN.68-66-B.SDR DHL2000720001Switch · out of adjON TAKEOFF, FWD ENTRY DOOR LIGHT ILLUMINATED. RETURNED TO MIA. ADJUSTED DOOR SWITCH, OPS CHECK GOOD PER MM 52-11-01.SDR DHL200072616CSkin · flakingA/C BAY ACCESS DOOR NR 3355L HAS EXTERNAL SURFACE COATING FLAKING. INSTALLED FILLER REPAIR AS PER SRM 51-40-1.SDR DHL200072622CFitting · damagedRT ELEVTOR TAB NR 3 HINGE FITTING AT ELEVATOR REAR SPAR HAS RADIAL PLAY. REMOVED AND REPLACED NR 3 HINGE BUSHING FITTING AT RT ELEVATOR PER M/M 27-30-01.SDR DHL200072627CBracket · crackedJUST BELOW NR 10 SPOILER BRACKET CRACKED AT ATTCH TO SPAR AREA WS.200.0. REMOVED AND REPLACED SPOILER BRACKET ON NR 10 SPOILER TO SPAR AREA PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072615CSkin · crackedLOWER FUSELAGE EXTERIOR RT SIDE OF AFT CARGO DOOR HAS AN AREA OF CORROSION AND CRACKED PAINT. INSTALLED FILLER REPAIR PER SRM 51-40-1 FIG 1.SDR DHL200072611CSeat Track · wornSEAT TRACK LOCK LUGS WORN RBL 48 AT STA 700. CUT OUT DAMAGED SECTION OF SEAT TRACK RBL 48 FROM STA 690 TO 720 PER SRM 53-10-5. INSTALLED NEW SEAT TRACK PER SRM 53-10-5. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072610CSeat Track · wornSEAT TRACK LOCK LUGS WORN STA 600 RBL 24. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-2.SDR DHL200072605CAngle · brokenMAIN ENTRY DOOR AFT LOWER CORNER HAS ANGLE SUPPORT BROKEN. MAIN ENTRY DOOR LOWER CORNER REMOVED AND REPLACED ANGLE SUPPORT PER SRM 51-40-3 & 51-10-6. TREATED AND PRIMED PER SRM 51-10-2.SDR DHL200072604CSeat Track · wornSEAT TRACK LOCK LUGS WORN RBL 48 STA 760. SMOOTHED OUT AREA AT STA 760 RBL 48 PER SRM 51-10-1. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 3. REMOVED SEAT TRACK AT RBL 48 STA 760 PER SRM 51-30-2. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 FIG 2. ALODINED SDR DHL200072601CSeat Track · wornSEAT TRACK LOCK LUGS WORN RBL 48 FROM STA 1160 TO 1170. REPLACED SEAT TRACK ON RBL 48 FROM STA 1160 TO 1170 PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072625CSeat Track · wornSEAT TRACK BL 0 LOCK LUGS WORN AT STA 849. REMOVED SEAT TRACK PER SRM 51-30-2. INSTALLED SEAT TRACK PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072624CSeat Track · wornSEAT TRACK LBL 24 FROM STA 390 TO APPROX STA 398 LOCK LUGS WORN. REMOVED SEAT TRACK PER SRM 51-30-2. INSTALLED NEW SEAT TRACK PER SRM 51-30-2 AND 53-10-5 FIG 1. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072623CSeat Track · wornSEAT TRACK LBL 24 FROM STA 520 TO STA 540 LOCK LUGS WORN. REMOVED SEAT TRACK FROM STA 480 TO STA 560 LBL 24 PER SRM 51-30-2. INSTALLED NEW SEAT TRACK PER SRM 51-30-2 & 53-10-5 FIG 7. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200019CSeat Track · wornSEAT TRACK LOCK LUGS WORN BL 0 STA 698 TO 705. REMOVED CABIN SEAT TRACK BL 0 FROM STA 680 TO 720 PER SRM 51-30-2. INSTALLED SEAT TRACK PER SRM 51-30-2 & 53-10-5. TREATED AND PRIMED PER SRM 51-10-2.SDR DHL200072626CCowling · brokenNR 1 ENG NOSE COWL AFT AREA APPROX 9 O''''CLOCK POSITION HAS A PIECE OF SKIN BROKEN. REMOVED EXISTING REPAIR PER SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR PER SRM 51-10-2.SDR DHL200072621CSkin · crackedNR 1 ENG UPPER COWL I/B SIDE FWD LATCH AREA WORN SKIN CRACKED. REMOVED DOUBLER REPAIR AT NR 1 ENG UPPER COWL FWD LATCH AREA PER SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR PER SRM 54-10-3 FIG 5. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM SDR DHL200072620CSkin · crackedNR 1 ENG LOWER COWL EXT SKIN I/B SIDE FWD HINGE AREA CRACKED. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER REPAIR PER SRM 54-10-3 FIG 5. ALODINED AND PRIMED PER SRM 51-10-7.SDR DHL200072631CChannel · damagedRET STABILIZER RT SIDE UNDER THE SLIDING PLATE IS DAMAGED ON THE FRONT CHANNEL. REMOVED THE SLIDING PLATE IAW SRM 51-30-2. REMOVED CHANNEL AND MANUFACTURED AND INSTALLED NEW CHANNEL PER SRM 51-10-1. REINSTALLED SLIDING PLATE PER SRM 51-30-2.SDR DHL200072628CAngle · crackedLOWER T/E PANEL WS 536 APPROX ANGLE SUPPORT CRACKED. REMOVED AND REPLACED LOWER OUTBOARD T/E ANGLE SUPPORT PER SRM 57-30-2. INSTALLED PHENOLIC BLOCK AT LOWER T/E PER SRM 51-30-2.SDR DHL200072617CAngle · crackedNR 7 SLAT O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. REMOVED CRACKED ANGLE FROM NR 7 SLAT O/B TRACK TO SLAT ATTACH ANGLE PER SRM 51-30-2. REPLACED ANGLE PER SRM 51-30-2 & 51-10-2 FIG 4.
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