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 DHL200072436CAccess Panel · delaminatedAT C CHECK, FOUND LT WING LOWER TE PANEL BELOW NR 3 SPOILER DELAMINATED. REMOVED PANEL, INSTALLED FIBERGLASS REPAIR, REINSTALLED PANEL.SDR DHL200072427CSkin · corrodedAT C CHK FOUND FWD CARGO BAY. CORROSION AT SKIN JUST FWD OF FRAME STA 520 & STR 19 RT. REMOVED FASTNERS AND DAMAGED SECTION, REMOVED CORROSION AT FUSELAGE SKIN, FOUND OUT OF LIMITS. REMOVED DAMAGED SECTION OF STRINGER 19 RT FROM STA 486, STA 535. REMOVESDR DHL200072422CFrame · crackedAT C-CHECK, FOUND RT SIDE OF AFT FUSELAGE STATION FS 1186 STRINGER 26R HAS A CRACK RUNNING FROM A RIVET TO A HI-LOK AND OUT OF THE HI-LOK HOLE. AREA IS AT THE RT SIDE OF THE DOOR CUTOUT FOR AFT STAIR HANDLE OPERATING MECHANISIM. CUT OUT DAMAGED SKIN AREA PERSDR DHL200072421CKeelbeam · chafedAT C-CHECK, FOUND PLATE TO KEEL BEAM TOP SIDE UNDER THE APU LOWER SIDE IS CHAFED THROUGH BY THE APU. REMOVED AND FABRICATED PLATE AT KEEL BEAM TOP SIDE UNDER THE APU LOWER SIDE. TREATED AND PRIMED AREA AS PER SRM 51-30-2. INSTALLED KEEL BEAM PANELS PER M/M SDR DHL200072420CBulkhead · crackedAT C-CHECK FOUND LEFT SIDE OF THE AFT PRESSURE BULKHEAD FS 1183 HAS A CRACK RUNNING FROM A LIGHTNING HOLE UPWARD ON VERTICAL BEAM AT BL 26L AND WL 54N ABOVE FLOOR. STOP DRILLED CRACK ON VERTICAL BEAM BL26L AND WL 54 IN ABOVE FLOOR IAW B727 SB 53-0182. PERFORSDR DHL200072413CAngle · brokenAT C-CHECK, FOUND LEFT WING T/E LOWER PANEL SUPPORT BROKEN AT WING STA 542. REMOVED AND REPLACED BROKEN ANGLE SUPPORT (P/N 65-21658-27) LEFT WING T/E PANEL AT WING STA 543.68 AS PER BOING 727 SRM 51-30-2. CHECKED ROD ADJUSTMENT FOR COVE PANEL AND FORE FLAP CSDR DHL200072412CSupport Bracket · crackedAT C-CHECK, FOUND LEFT WING T/E LOWER PANEL SUPPORT BRACKET CRACKED AT WING STATION 520. REMOVED AND REPLACED LEFT WING T/E LOWER COVE PANEL SUPPORT ANGLE (P/N 65-21658-30) AT WING STA 521.53 AS PER BOEING 727 SRM 51-30-2. CHECK ROD ADJUSTMENT FOR COVE PANELSDR DHL200072414CAngle · crackedAT C-CHECK, FOUND LEFT WING LOWER PANEL SUPPORT BRACKET CRACKED AT WING STA 566. REMOVED AND REPLACED LEFT WING T/E LOWER COVE PANEL SUPPORT ANGLE (P/N 65-21658-25) AT WING STA 567 AS PER BOING 727 SRM 51-30-2. CHECKED ROD ADJUSTMENT FOR COVE PANEL AND FORE SDR DHL200072411CSupport Bracket · crackedAT C-CHECK, FOUND LEFT WING T/E LOWER PANEL SUPPORT BRACKETS CRACKED AT WING STA 500. REMOVED AND REPLACED LEFT WING T/E LOWER COVE PANEL SUPPORT ANGLES AT WING STA 498.08 PER BOEING SRM 51-30-2. CHECKED ROD ADJUSTMENT FOR COVE PANEL AND FORE FLAP CLEARANCE SDR DHL200072409CSkin · delaminatedAT C-CHECK, FOUND RT WING LOWER ACCESS PANEL 8613 DELAMINATED AND HAS CORROSION.INSTALLED BONDED REPAIR AT RT WING LOWER PANEL 8613 PER B 727 SRM 51-40-6 FIG 1. INSTALLED PANEL PER M/M 12-31-00.SDR DHL20007247CSkin · damagedAT C-CHECK, FOUND FWD PASSENGER DOOR EXTERIOR SKIN HAS PIECE BROKEN OUT AT EDGE JUST ABOVE TOP HINGE ARM. REMOVED FASTENERS PER SRM 51-30-2. ROUTED OUT CRACK IAW SRM 51-10-1 FIG 2. INSPECTED ROUTED AREA IAW NDT MM 51-00-00 PART 6 FIG 4 NO CRACK INDICATION. SDR DHL200072406CTail Cone · puncturedAT C-CHECK, FOUND VERTICAL FIN TAIL CONE ASSY PUNCTURED IN SEVERAL PLACES ON LOWER HALF. REMOVED TAIL CONE IAW B72755-30-41. INSTALLED FIBERGLASS OVERLAY REPAIR AS PER BOEING M/M 51-40-8 FIG 1. USED FIBERGLASS CLOTH STYLE 7781 P/O 931150556 EPOCAST RESIN 5SDR DHL200072401CSkin · crackedAT C-CHECK, FOUND LEFT I/B MID FLAP INNER SURFACE AFT PANEL CRACKED AT O/B END OF FLAP AROUND SCREW HOLE. CUT OUT DAMAGED AREA AT LEFT I/B MID FLAP LOWER SURFACE, AFT PANEL, O/B END OF FLAP AROUND SCREW HOLE AS PER AVRTOS EO NR AYHM-115RO-1. INSTALLED EXTERNSDR DHL200072424CDoubler · crackedAT C-CHECK, FOUND LEFT WING REAR SPAR LOWER CHORD, CORRUGATED DOUBLER CRACKED AT WING STATION 522. REMOVED AND REPLACED CORRUGATED DOUBLER AT LT WING REAR SPAR LOWER CHORD WS 522 AS PER 727 SRM 51-10-1.SDR DHL200072423CSensor · malfunctionedAT C-CHECK, FOUND BROKEN FLIGHT RECORDER AILERON SURFACE POSITION SENSOR. REMOVED AND REPLACED DFDR AILERON POSITION SENSOR PER FLIGHT SYSTEMS ENG DWR 7277342121. ADJUSTED DFDR AILERON POSITION SENSOR PER FLIGHT SYSTEMS ENG REPORT NR 95-03-27. CHECKED DFDR SDR DHL200072479CDoubler · crackedAT C CHECK, FOUND CORROGATED DOUBLER AT SPAR LOWER CHORD, CRACKED LT WS 544. REMOVED AND REPLACED CORROGATED DOUBLER AT REAR SPAR LOWER CHORD LT WS 544 PER SRM 51-10-1.SDR DHL200072475CAngle · crackedAT C CHECK, FOUND SUPPORT ANGLE CRACKED AT RT WING FWD SPAR UPPER CHORD 2 INCHES I/B OF SLAT STA 0. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2.SDR DHL200072472CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL SUPPORT CHANELS AT WS 521.53 ARE CRACKED AND BROKEN. REPLACED COVE PANEL SUPPORT CHANELS PER SRM 51-30-2.SDR DHL200072471CAngle · wornAT C CHECK, FOUND RT WING TE COVE PANEL SUPPORT ROD AT WS 543.68 UPPER ATTACH ANGLE WORN, ROD IS LOOSE. REMOVED AND REPLACED ANGLES PER SRM 51-30-2.TREATED AND PRIMED AREA PER SRM 51-10-2.SDR DHL200072470CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL I/B SUPPORT CHANEL AT WS 567 CRACKED. REMOVED AND REPLACED SUPPORT CHANEL PER SRM 51-30-2.SDR DHL200072469CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL O/B SUPPORT CHANEL WS 447.90 CRACKED. REPLACED SUPPORT CHANEL PER SRM 51-10-1 PARA 4 & 51-30-2.SDR DHL200072468CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL INBD SUPPORT CHANEL AT WS 469.93 CRACKED. REMOVED OLD SUPPORT CHANEL PER SRM 51-30-2. INSTALLED NEW CHANEL PER SRM 51-30-2.SDR DHL200072467CPanel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL SUPPORT CHANELS AT WING STA. 498 ARE CRACKED. REMOVED AND REPLACED WITH NEW SUPPORT CHANELS PER SRM 51-30-2.SDR DHL200072466CAngle · crackedAT C CHECK, FOUND RT WING TE SMALL LOWER SUPPORT ANGLE ON THE FWD SIDE OF THE NR 8 SPOILER ACTUATER FITTING CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-6.SDR DHL200072460CPanel · delaminatedAT C CHECK, FOUND LT PRIMERY HEAT EXCHANGER PANEL REAR AREA SHOWS DELAMINATION. INSTALLED FIBERGLASS OVERLAY REPAIR AT LT PRIMARY HEAT EXCHANGER PANEL REAR PER SRM 51-40-8 FIG 1SDR DHL200072447CSeat Track · wornDURING C CHECK FOUND NR 3 SEAT TRACK, LBL.24. LOCK TAB WORN AT STA 520. REMOVED NR 3 SEAT TRACK LBL 24 AT STA 520. PER SRM 51-30-2, REPLACED NR 3 SEAT TRACK LBL 24 AT STA 520 PER SRM 51-30-7, TREATED AND PRIMED PER SRM 51-10-2.SDR DHL200072446CSeat Track · wornAT C CHECK, FOUND NR 4 SEAT TRACK BL 0 HAS WORN LOCK TABS AT APPROX STA 532 & 552. REMOVED AND INSTALLED NEW SEAT TRACK NR 4, BL 0, FROM BS 480 TO BS 560 PER SRM 53-10-5 FIG 7, ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072445CSeat Track · corrodedFOUND AT C CHECK, CORROSION ON NR 4 SEAT TRACK BL 0 ON UPPER SURFACE APROX 12 INCHS FWD OF STA 720C. REMOVED NR 4 SEAT TRACK BL.0 FROM STA 720 TO 720F. PER SRM 51-30-2, INSTALLED NEW SEAT TRACK AT BL 0 FROM STA 720 TO 720F PER SRM 51-30-2, ALODINED AND PRSDR DHL200072444CSeat Track · wornAT C CHECK, FOUND SEAT TRACK NR 5, RBL 24 HAS WORN LOCK TABS AT STA 990. REMOVED FLOOR PANELS FROM STA 950 TO 990 FOR ACCSESS, CUT OUT DAMAGED SECTION OF SEAT TRACK PER SRM 53-10-5 FIG 7, INSTALLED NEW SEAT TRACK AS PER SRM 53-10-5 FIG7, ALODINED AND PRISDR DHL200072431CAngle · crackedAT C CHK FOUND NR 6 LE SLAT O/B TRACK ROLLER SUPPORT WEB O/B VERTICAL ATTACH ANGLE IS CRACKED BETWEEN FASTNERS AT LOWER SPAR CHORD. CLEANED AREA NR 6 LE SLAT O/B TRACK ROLLER SUPPORT WEB O/B VERTICAL ATTCH ANGLE BETWEEN FASTNERS AT LOWER SPAR CHORD PER SRM 51SDR DHL200072425CShift Mechanism · failedAT C-CHECK, FOUND NOSE LANDING GEAR GROUND SHIFT MECHANISM LINKAGE ASSY HAS CRACK. REMOVED AND REPLACED NOSE LANDING GEAR GROUND SHIFT MECHANISM LINKAGE ASSY BRACKET PER M/M 32-21-0. ACCOMPLISHED ADJUSTMENT OF THE NOSE LANDING GEAR GROUND SHIFT MECHANISM PERSDR DHL200072461CAccess Panel · delaminatedAT C CHECK, FOUND LOWER FUSELAGE ACCESS PANEL 3355 RT SHOWS DELAMINATION. INSTALLED FIBERGLASS OVERLAY REPAIR AS PER SRM 51-40-8 FIG 1.SDR DHL200072474CAngle · crackedAT C CHECK, FOUND RT WING LE RIB ATTACH ANGLE CRACKED AT SLAT STA 0. REMOVED AND REPLACED RT WING RIB ATTACH ANGLE PER SRM 51-40-3 AND 51-30-2.SDR DHL200072430CAngle · crackedAT C CHECK FOUND NR 7 LE I/B SLAT TRACK ROLLER SUPPORT WEBS I/B & O/B ATTACH ANGLES ARE CRACKED AT LOWER SPAR CHORD. REMOVED I/B & O/B VERTICAL ANGLES ON & NR 7 LE PER SRM 51-30-2. FABRICATED NEW ANGLES PER SRM 57-10-1 FIG 1. ALODINED AND PRIMED AREA & PARTSSDR DHL200072482CAngle · brokenAT C CHECK, FOUND LT WING TE PANEL AT WS 491 TO 519 HAS A BROKEN ATTACH ANGLE ON INBD SIDE BELOW NR 3 SPOILER. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-2.SDR DHL200081CAngle · brokenAT C CHECK, FOUND LT WING TE PANEL AT WS 491 TO 519, HAS A BROKEN ATTACH ANGLE ON O/B SIDE. PANEL IS BELOW NR 3 SPOILER. REMOVED AND REPLACED ANGLES AT LT WING TE PANELS AT WS 491 TO 519 PER SRM 51-30-2.TREATED AND PRIMED PER SRM 51-10-2.SDR DHL200072480CPanel · crackedAT C CHECK, FOUND LT WING TE PANEL BELOW THE NR 2 SPOILER CRACKED ATTACH ANGLES ON O/B SIDE. REMOVED AND REPLACED WITH NEW ANGLES AT LT WING TE PANEL BELOW NR 2 SPOILER ON O/B SIDE PER SRM 51-30-2.SDR DHL200072443CTube · crackedAT C CHECK, FOUND NR 2 ENGINE RT FWD COWL, END OF DRAIN TUBE AREA SHOW SKIN CRACKED. INSTALLED EXTERNAL DOUBLER REPAIR AT NR 2 ENGINE RT FWD COWL END OF DRAIN TUBE AREA PER SRM 54-10-3 FIG6. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200072442CSkin · erodedFOUND DURING C CHECK, NR 2 ENGINE RT COWL, LOWER SKIN AFT MIDDLE SECTION IS ERODED. INSTALLED EXTERNAL DOUBLER REPAIR AT NR 2 ENGINE RT FWD COWL PER SRM 54-10-3 FIG 6. ALODINED AND PRIMED PER SRM 51-10-2SDR DHL200072439CHinge · crackedAT C CHECK, FOUND RT WW DOOR I/B SECTION, CENTER FWD HINGE CRACKED. REMOVED AND REPLACED WITH NEW CENTER FWD HINGE AT RT WW DOOR I/B SECTION. OPS CHECKED PER MM 32-30-00.SDR DHL200072438CHinge · crackedFOUND AT C CHECK, RT WHEEL WELL DOOR I/B SECTION OF HINGE IS CRACKED. REMOVED AND REPLACED WITH NEW AFT HINGE AT RT WW DOOR I/B SECTION. OPS CHECKED.SDR DHL200072437CAngle · crackedFOUND AT C CHECK, LT WING TE PANEL BELOW NR 2 SPOILER HAS CRACKED ATTACH ANGLES ON I/B SIDE. REMOVED AND REPLACED WITH NEW ANGLE AT LT WING TE PANEL BELOW NR 2 SPOILER.SDR DHL200072434CFairing · crackedAT C CHECK, FOUND LOWER FUSELAGE FAIRING CRACKED AT BS 740 AND ACCESS PANEL 3448R. RENOVED AND REPLACED DAMAGED SECTION OF FAIRING FRAME AT STA 740. ALODINE AND PRIMED AREA.SDR DHL200072433CAccess Panel · delaminatedAT C CHECK, FOUND LT WING LOWER ACESS PANEL 6803L, DELAMINATED. INSTALLED FIBERGLASS OVERLAY REPAIR, LT WING LOWER ACCESS PANEL 6803L.SDR DHL2000727001Web · cracked1 CRACK COMING OFF PREVIOUS DOUBLER REPAIR IN NOSE WHEEL WELL. REMOVED PREVIOUS REPAIR, INSTALL REPAIR DOUBLER PER SRM 53-10-4 AND S/B 53-65.SDR DHL200072102Controller · failedSMOKE EMITTED FROM ABOVE FD CONTROL HEAD. TROUBLE SHOT, INSPECTED WIRING UNDER CONSOLE AND FWD E/E. FOUND LIGHT PLATE BURNT ON FLIGHT DIRECTOR CONTROL PANEL. REPLACED A/P AMD F/D CONTROL PANELS. ALL CHECKS GOOD PER MM 22-11-101 AND MM 34-62-51.SDR DHL2000721002Controller · failedSMOKE EMITTED FROM ABOVE FD CONTROL HEAD. TROUBLE SHOT, INSPECTED WIRING UNDER CONSOLE AND FWD E/E. FOUND LIGHT PLATE BURNT ON FLIGHT DIRECTOR CONTROL PANEL. REPLACED A/P AMD F/D CONTROL PANELS. ALL CHECKS GOOD PER MM 22-11-101 AND MM 34-62-51.SDR DHL2000726001Skin · corrodedAT CHECK, STATION 660 WL 148, AREA OF CORROSION BETWEEN STRINGER 30L AND 30R. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-30-3 AND 53-10-4 AND DRAWING BY AERONAUTICAL SOLUTIONS ASI- 00-001IR. REPAIR 10 X 9.SDR DHL2000721001Skin · crackedFUSELAGE SKIN CRACK AT FWD ENTRY DOOR UPPER HINGE CUTOUT RADIUS. TRIMMED OUT CRACKED SECTION OF SKIN 1.75 X 1.5. INSTALLED DOUBLER REPAIR PER S/B 53-0198, DOUBLER 9 X 18, FILLER 9 X 6.SDR DHL99727006Switch · out of adjustMAIN CARGO DOOR LIGHT CAME ON IN FLIGHT THEN WENT OUT. ADJUSTED AFT AUX LATCH PIN SWITCH PER PEMCO M 52-32-21 PRESSURIZED AIRCRAFT AND OPS CHECKED GOOD.
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