Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 DHLA2009743DH584Floorbeam · damagedUPPER FUSELAGE MAIN CARGO CABIN BS 320 LBL 63 FLOORBEAM UPPER CHORD WITH DOUBLE HOLE. REPAIRED FLOORBEAM AT BS 380 BETWEEN LBL52.5 AND LBL 64 IAW EC NR COO-2-53-426-08 DOCUMENTED ON FORM 8110-3.SDR DHLA2009743DH580Floorbeam · damagedUPPER FUSELAGE MAIN CARGO CABIN STA 540 RBL62 FLOORBEAM UPPER CHORD WITH DOUBLE HOLE. REPAIRED FLOORBEAM UPPER CHORD SECTION AT BS 540 FROM RBL 53 TO RBL 70 IAW EO NR COO-2-53-471-08 DTD 12/17/08 DOC.SDR DHLA2009743DH578Skin · damagedUPPER FUSELAGE CARGO CABIN FROM BS 500 TO BS 645 MISSING FASTENERS ON S-3L. INSTALLED SOLID RIVETS FROM BS 500 TO BS 645 S-3L DUE TO OPEN FASTENER HOLES NOT CAPTURED IAW B727 SRM 51-30-2 AND PEMCO WORLD AIR SERVICE ENGINEERING AUTHORIZATION NR PD27-53-128 DTDSDR DHLA2009743DH576Seat Track · crackedUPPER FUSELAGE CARGO CABIN STA 618 LBL 45 SEAT TRACK LOWER SECTION CRACKED. REPLACED SEAT TRACK SECTION BTWN BS 560 AND BS 690 AT LBL 45 IAW SRM 51-10-1 PARA 7A.SDR DHLA2009743DH566Skin · wornEMPENNAGE VERTICAL STABILIZER LOWER RUDDER L/E LT AND RT SIDES WITH WEAR DUE TO CHAFING AGAINST RUB SEAL. REPAIRED LWR RUDDER FROM RUD STA 60.387 TO RUD STA 154.185 RT AND FROM RUD STA 81.983 TO RUD STA 154.185 LT IAW B727 SRM 55-40-3 FIG 1.SDR DHLA2008743510Floorbeam · corrodedUPPER FUSELAGE CARGO CABIN BS 312 BETWEEN RBL 41 TO LBL 45 FLOORBEAM UPPER CHORD WITH CORROSION AT BOTH SECTIONS. REPAIRED FLOORBEAM SECTION AT BS 312 BETWEEN LBL 9 TO RBL 63 IAW B 727 SRM 53-10-8 FIG 9.SDR DHLA2008743508Floorbeam · corrodedUPPER FUSELAGE CARGO CABIN BS 380 AT LBL 38 AND BETWEEN RBL 53 AND 64 FLOORBEAM CORRODED BETWEEN RBL 53 AND RBL 64. REMOVED CORROSION AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-10-1 FIG 5. REPAIRED FLOORBEAM SECTION AT BS 380 BTWN LBL 29.5 AND LBL 48SDR DHLA2008743507Frame · damagedUPPER FUSELAGE CARGO CABIN BS 328 BTWN S-13R AND S-14R FRAME INBD FLANGE AND SUPPORT ANGLE WITH DOUBLE HOLE AND BTWN S-16R AND 17R ELONGATED HOLES. REPAIRED FRAME AT BS 328 BTWN S-13R AND 18R IAW B727SRM 51-40-4 FIG 1.SDR DHLA2009743DH669Frame · dentedUPPER FUSELAGE MAIN CARGO CABIN AT BS 360 BTWN S-7L AND S-8L FRAME INBD FLANGE WITH DENT. REPAIRED FRAME SECTION AT BS 360 BTWN S-7L AND S-9L IAW EO COO-2-53-430-08 DTD 11/24/08 DOCUMENTED ON FAA FORM 8110-3.SDR DHLA2009743DH660Frame · damagedUPPER FUSELAGE MAIN CARGO CABIN AT BS 378 BTWN S-16R AND S-17R FWD GALLEY DOOR FRAME WITH HOLE LOCATED ON FRAME RATIO. REPAIRED FRAME SECTION AT BS 376 BTWN S-16R AND S-17R IAW COOPESA EO COO-2-53-441-08 DTD 12/04/08 DOCUMENTED ON FAA FORM 8110-3.SDR DHLA2008743DH619Frame · damagedUPPER FUSELAGE MAIN CARGO CABIN AT BS 480 BETWEEN S-7L AND S-8L SIDE FRAME WEB WITH DOUBLE HOLE. REPAIRED FRAME AT BS 480 BETWEEN S-6L AND S-9L IAW B737 SRM 53-10-4 FIG 1.SDR DHLA2008743521Frame · damaged"D" CHECK, UPPER FUSELAGE PAX CABIN AT BS 680 BETWEEN STR.16R & 17R FRAME WITH HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 680 BETWEEN S15 & 17R DUE TO DOUBLE HOLE IAW SRM 51-40-3 FIG.1.SDR DHLA2008743522Frame · crackedD-CHECK, WO NR 5740, NR 5740-2-136, UPPER FUSELAGE PAX CABIN AT BS 440 BETWEEN STR16R AND 17R FRAME INBD FLANGE WITH CRACK. REPAIRED FRAME AT BS 440 BETWEEN STR 15R AND 17R. DUE TO CRACK IAW SRM 51-40-3 FIG.1.SDR DHLA2008743515Strap · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 700 TO BS 720A WL 200 LBL47 STABILIZER STRAP WITH CORROSION OUT OF LIMITS. REPLACED STABILIZER STRAP FROM BS 680 TO BS 720C WL 200 LBL 47 IAW B727 SRM 51-10-1 PARA 7A.SDR DHLA2008743504Skin · wornLT WING OTBD FORE FLAP L/E LOWER SURFACE WITH WEAR AT WBL 492. REPAIRED L/E SKIN SECTION AT OTBD FORE FLAP LT WING FROM WBL 492.5 TO WBL 482.5 IAW SRM 57-50-4 FIG 4.SDR DHLA2009743DH668Frame · damagedUPPER FUSELAGE MAIN CARGO CABIN AT BS 720F BTWN S-16L AND S-17L FRAME WITH DOUBLE HOLE. REPAIRED FRAME SECTION AT BS 720F BTWN S-15L AND S-17L IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009743DH667Frame · damagedUPPER FUSELAGE MAIN CARGO CABIN AT BS 1090 BTWN S-10R AND S-14R FRAME INBD FLANGE WITH ELONGATED HOLES. REPAIRED FRAME SECTION AT BS 1090 BTWN S-10R AND S-14R IAW B727 SRM 53-10-4 FIG 1.SDR DHLA2009743DH657Stringer · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 950A TO BS 950C S-21L WITH CORROSION. REPAIRED STRINGER SECTION FROM BS 950+8" TO BS 950C-5" AT S-21L IAW SRM 53-10-3 FIG 1.SDR DHLA2009743DH652Frame · dentedUPPER FUSELAGE MAIN CARGO CABIN AT BS 360 BTWN S-4R AND S-5R FRAME INBD FLANGE WITH DENT. REPAIRED FRAME SECTION AT BS 360 BTWN S-4R AND S-6R IAW COOPESA EO COO-2-53-430-08 DTD 11/24/08 DOCUMENTED ON FAA FORM 8110-3.SDR DHLA2009743DG627Skin · crackedNR 1 ENG NOSE COWL AT NAC STA 68 OUTER SKIN WITH CRACK BETWEEN 5 AND 6 O`CLOCK POSITION. REPAIRED LIP SKIN OUTER SIDE BETWEEN 5 AND 6 O`CLOCK POSITION IAW COOPESA EO COO-2-54-452-08 DTD 12/08/08 DOCUMENTED ON FAA FORM 8110-3.SDR DHLA2009743DH575Frame · damagedUPPER FUSELAGE CARGO CABIN AT BS 540 BTWN S-14R AND S-17R FRAME WITH DOUBLE HOLES. REPLACED FRAME SECTION BS 540 BTWN S-13R AND S-25R IAW B727 SRM 51-10-1 PARA 7A.SDR DHLA2009743DH563Frame · damagedUPPER FUSELAGE CARGO CABIN AT BS 720F BTWN S-16L AND S-17L FRAME WITH DOUBLE HOLE. REPAIRED FRAME SECTION AT BS 720F BTWN S-15L AND S-17L IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009743DH561Frame · dentedLOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 1050 BTWN S25R AND S27R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 1050 BTWN S23R AND S27R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009743DH560Frame · dentedUPPER FUSELAGE CARGO CABIN AT BS 720B BTWN S-16L AND S-17L FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 720B BTWN S-15L AND S-17L IAW SRM 51-40-3 FIG 1.SDR DHLA2009743DH559Frame · damagedUPPER FUSELAGE CARGO CABIN BS 720D BTWN S-16L AND S-17L WITH HOLE. REPAIRED FRAME SECTION AT BS 720D BTWN S-15L AND S-17L IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009743DH558Frame · damagedUPPER FUSELAGE CARGO CABIN AT BS 720E BTWN S-16L AND S-17L FRAME WITH DOUBLE HOLE. REPAIRED FRAME SECTION AT BS 720E BTWN S-15L AND S-17L IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2009743DH556Frame · dentedUPPER FUSELAGE CARGO CABIN AT BS 660 BTWN S-16R AND S-17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 660 BTWN S-13R AND S-21R IAW B727 SRM 51-40-3 FIG 1.SDR DHLA2008743523Frame · damagedD-CHECK AT WO NR 5740, NR 5740-2-115, UPPER FUSELAGE PAX CABIN BS 620 BETWEEN STR 16R AND 17R FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 620 BETWEEN STR 15R AND 17R DUE TO DOUBLE HOLE.SDR DHLA2008743528Frame · dentedD-CHECK, WO NR 5740, NR 5740-1-137 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 970 STR 26L FRAME WITH DENT. REPAIRED FUSELAGE SECTION AT BS970 BETWEEN STR.25L AND 27L DUE TO DENT IAW SRM 51-40-3 FIG.1SDR DHLA2008743526Frame · damagedD-CHECK, WO NR 5740, NR 5740-2-85, UPPER FUSELAGE PAX CABIN STA 1090 BETWEEN STRINGERS 10 AND 11, 13 AND 14 RT FRAME INBD FLANGE WITH ENLONGATED HOLES. REPAIRED FUSELAGE FRAME SECTION AT BS1090 BETWEEN STR 10R AND STR 14R DO TO ELONGATED HOLES IAW SRM 53-10-4SDR DHLA2008743525Frame · dentedD-CHECK, WO NR 5350 NR 5350-2-98, UPPER FUSELAGE PAX CABIN AT BS 700 STR 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 700, BETWEEN STR 16R AND STR 17R DUE TO DENT IAW SRM 51-40-3 FIG.1.SDR DHLA2008743505Frame · damagedUPPER FUSELAGE CARGO CABIN AT BS 580 BETWEEN S-14R AND S-17R FRAME WITH DENT AND DOUBLE HOLE. REPLACED FRAME SECTION AT BS 580 BETWEEN S-12R AND S-18R DUE TO DOUBLE HOLES IAW B727SRM 51-10-1 PARA 7D.SDR DHLA2009743DH567Angle · crackedRT WING INBD MID FLAP TRAILING EDGE SECTION, LOWER SUPPORT ANGLE WITH CRACKS AT WBL 112. REPAIRED INBD MID FLAP T/E SECTION LOWER SUPPORT ANGLE BETWEEN WBL70.59 AND WBL249.3 IAW SRM 51-40-4 FIG 1.SDR DHLA2009743DH588Skin · wornRT WING INBD FORE FLAP OTBD END LEADING EDGE SKIN WITH WEAR. REPAIRED RT INBD FORE FLAP FROM WBL 249.3 TO WBL 240 IAW SRM 57-50-4 FIG 4.SDR DHLA2009743DH562Frame · damagedUPPER FUSELAGE CARGO CABIN AT BS 910 BTWN S-4L AND S-5L FRAME WEB WITH DOUBLE HOLES. REPAIRED FRAME SECTION AT BS 910 BTWN S-2L AND S-7L IAW B727 SRM 53-10-4 FIG1.SDR DHLA2008743527Frame · damaged"D" CHECK, UPPER FUSELAGE PAX CABIN BS 1090 BETWEEN 13L & 14L FRAME I/B FLANGE WITH DOUBLE HOLES & DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 1090 BETWEEN STR. 11L & STR.14L DUE TO DOUBLE HOLES & DENT IAW SRM 53-10-4 FIG.1SDR DHLA2009743DH664Support Beam · damagedRT WING TRAILING EDGE MAIN LANDING GEAR SUPPORT BEAM AFT LOWER FLANGE WITH DOUBLE HOLE AT WS 251. REPAIRED RT MLG SUPPORT BEAM LOWER FLANGE AT WS 251 IAW COOPESA EO COO-2-57-436-08 DTD 11/28/08 AND BOEING MESSAGE NR 1-1087194336-2 DTD 11/26/08 DOCUMENTED ON FSDR 08FDEA04792Skin · dentedSKIN DENTED AT LAP SEAM STA 1115 STR 20R. EVALUATED DENT AND FOUND OUT OF LIMITS, REMOVED DAMAGED SKIN DIMS 3.3 INCH BY 1.8 INCH. FABRICATED FILLER 3.3 INCH BY 1.8 INCH, DOUBLER 12.250 INCH BY 8.5 INCH IAW SRM 53-30-3 FIG 24. INSTALLED REPAIR PARTS IAW SRSDR 08FDEA04793Skin · misrepairedPREVIOUS REPAIR AT STA 188 STR 26L HAS 1 DENT AND NUMEROUS IMPROPERLY INSTALLED FASTENERS. REMOVED DOUBLER, FABRICATED NEW DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 51-30-5, 53-30-2 AND 53-30-3.SDR FDEA200811054728Switch · misalignedNR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOOD FOR SERVICE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4.SDR DHLA2008743516Strap · corrodedUPPER FUSELAGE CARGO CABIN BS 720C+3 INCH AT LBL 2 AND LBL 25 FLOORBEAM STABILIZER STRAPS CORRODED. REPLACED STABILIZER STRAP LBL2 FROM BS 720C TO BS 720F IAW B727 SRM 51-10-1 PARA 7A. REMOVED CORROSION AND FOUND WITHIN LIMITS ON STABILIZER STRAP BS 720C+3 ISDR 08FDEA04728Switch · misalignedNR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOOD FOR SERVICE. PREMATURE REMOVAL/INSTALLATION. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4SDR FDEA200810244538Bypass Valve · leakingDURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A ALT FLAPS AND MANUAL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPLACED RT FLAP BYPASS VALVESDR 08FDEA04538Valve · leakingDURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A. ALT FLAPS AND MANUAL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPLACED RT FLAP BYPASS SDR 08FDEA04514Switch · failedON DEPARTURE WHEN FLAPS RAISED FROM 5 TO O GOT AN LED DISAGREE LIGHT WITH NR 2 LE FLAP LED INDICATING NOT IN PROPER POSITION. REMOVED NR 2 LE FLAP SWITCH AND PIGGY BACKED ONTO NR 1 LE FLAP POSITION AND PROBLEM FOLLOWED. REINSTALLED CONNECTOR ON ORIGINAL NR SDR 08FDEA04322Seat Track · corrodedCORROSION ON SEAT TRACK BS 950 LBL 24. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED, LOCATED, DRILLED, AND DEBURRED SEAT TRACK IAW SRM 53-10-5 AND 51-30-5 AND 51-30-8. TREATED & PRIMED TRACK & REPAIR PARTS IAW SRM 51-10-2. INSTALLED SEAT TRACK & REPAISDR 08FDEA04321Seat Track · corrodedCORROSION SEAT TRACK STA. 950 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK AND 2 SPLICE ANGLES IAW SRM 53-10-5 FIG 1 AND 51-30-8. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED TRACK & REPAIR PARTS IAW SRM 53-10-5 & 51-30-5, ANDSDR 08FDEA04298Skin · dentedSKIN DENTES AND HOLES BS 620 TO 635 S25R.SDR CA081016004Hose · leaking(CAN) DURING DEPARTURE OF THE ACFT PRIOR TO ENGINE START, FUEL WAS NOTICED LEAKING FROM NR 3 ENGINE. MX REQUESTED NORMAL ENGINE START TO VERIFY FUEL LEAK. ENGINE WAS SHUT DOWN, AND ACFT TOWED BACK TO GATE FOR FURTHER INVESTIGATION. THE FUEL HOSE ASSEMBLY WASDR CA081122001Bulkhead · cracked(CAN) DURING WALK-AROUND INSP, FOUND BELTFRAME AT 9G BULKHEAD CRACKED BY LT CARGO CAN CUTOUT. TEMPORARY REPAIR CARRIED OUT. A/C FERRIED. PERMANENT REPAIR CARRIED OUT. ACFT RETURNED TO SERVICE.
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