Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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 = '727233' 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 07FDEA05098Spar · crackedVERTICAL STAB TIP L/E SPAR, CLOSER WEB HAS CRACK RUNNING THROUGH UPPER MOST FASTENER HOLE OF RIGHT SIDE TERMINAL FITTING LOCATION, 4.5" RBL. FABED DOUBLER, APPLIED ALODINE AND PRIMER AND INSTALLED REF DWG 65-17484, SRM 51- 10-2. CLASSIFIED AS A MINOR REPAIRSDR 07FDEA05097Stringer Clip · crackedSTRINGER CLIP IS CRACKED AT STATION 680, STRINGER 10 RIGHT REMOVED, FABRICATED, TREATED AND PRIMED, IDENTIFIED AND INSTALLED STRINGER CLIP IAW SRM 51-10-2, 51-20-1PG 11, 51-30-2 PG4 BAC DWG 60-7232-2 AND FED EX GMM 7-0-1001 P1 ITEM 7B.SDR 07FDEA05096Longeron · crackedNR 1 ENG LWR COWL DOOR OB LONGERON IS CRACKED AT AFT HINGE CUT OUT. REMOVED, FABRICATED NEW INTERCOSTAL, SENT TO HEAT TREAT ON SNR NR N00829. TREATED AND PRIMED, COMPLETED INSTALLATION, REF SRM 51-30-2, 51-10-2 AND BAC DWG 65-19507.SDR 07FDEA05095Fairing · crackedNR 1 ENG INBOARD COWLING IS CRACKED THROUGH AT 3RD LATCH FROM THE FRONT (TOP SIDE). REMOVED DAMAGE AND REPAIRED WITH DOUBLER, APPLIED ALODINE AND PRIMER REF SRM 54-10-03, DWG SR27-71-007, 51-10-02, CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA05092Web · corrodedCORROSION ON DITCHING WEB FRAMES AT BS 720E AND BS 720F, RT OF MAIN CARGO BAY, WL 208, RBL 67. BLENDED CORROSION ON DITCHING WEB, FOUND TO BE OUT OF LIMITS. ORIGINAL .040", REMOVED .010 " REF SRM 53-10-1 DISPLACED SEAT TRACK FROM STA 720B - 745, RBL 67 REF SDR 07FDEA05091Retainer · crackedLT FWD OVERWING PRESSURE SEAL CORNER RETAINER ANGLE IS CRACKED. FABRICATED ANGLE REF BAC DWG 50-07978, HEAT TREATED, TREATED AND PRIMED REF SRM 51-10-2. INSTALLED RETAINER REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR.SDR 07FDEA05090Seat Track · corrodedCORROSION AROUND SEAT TRACK ATTACH SCREW, BS 720E, RBL 64, WL 208. REMOVED DAMAGE SECTION OF SEAT TRACK, REF SRM 51-30-2 FROM STA 720-750, RBL 64. REMOVED CREASE BEAM FROM STA 720C-740, RBL 64 REF SRM 51-30-2. FABRICATED SEAT TRACK, REPAIR PARTS, REF SRM 53SDR 07FDEA05089Bracket · crackedLT WING TO BODY FAIRING ATTACH BRACKET AT STR S-18A, BS 937 IS CRACKED REMOVED CRACKED BRACKET. FABRICATED NEW BRACKET, P/N 65-60789-9, FROM 2024T3 - .063". A TAG A 59659/ PO 1026484. TREATED AND PRIMED AND INSTALLED NEW BRACKET REF SRM 51-30-2 PG 2 AND 8 SSDR 07FDEA05088Floor Support · corrodedFWD LAV FLOOR STRUCTURE STA 312 RBL 41 SUPPORT ANGLE CORRODED ON LWR SURFACE. BLENDED CORROSION ON ANGLE. OUT OF LIMITS. REMOVED, FABRICATED NEW ANGLE AND INSTALLED REF BOEING DWG 65-17593, SRM 51-10-2, SRM 53-10-2 AND SRM 51-30-02. THIS IS AS A MINOR REPASDR 07FDEA05087Pan · corrodedCORROSION AROUND ATTACH FWD AND UNDER EDGES OF LAV SINK CABINET FLOOR PAN, BS 304 TO BS 315, RBL 13 TO RBL 41, WL 208. REMOVED CORRODED FLOOR PAN AND FABRICATED NEW PAN REF SRM 51-30-2 PG 3, AND SRM 53-20-1 PG 5 AND 12. TREATED AND PRIMED AND APPLIED TOP COASDR 07FDEA05086Attach Angle · crackedFWD LAV, I/B WALL, ATTACH ANGLE FROM WALL TO FLOOR STRUCTURE IS CRACKED, BS 315, RBL 15. REMOVED CRACKED ANGLE AND FABRICATED NEW SUPPORT ANGLE REF DWG 65-26173 AND SRM 51-30-2 PG 3. TREATED AND PRIMED AND APPLIED TOP COAT TO NEW ANGLE REF SRM 51-10-2 PG 1.SDR 07FDEA05056Rib · crackedC-2 PIT FWD CARGO DOOR HAS 2ND, 5TH AND 6TH LOWER EDGE FORMER RIBS CRACKED IN INSIDE OF DOOR REMOVED DAMAGE RIBS 3. FORMED 3 RIBS FROM 7075-0 .050". HEAT TREATED TO T-6, 3EA. TRANSFERRED FASTENERS HOLES, APPLIED ALODINE, PRIMER AND PAINT. INSTALLED 3 RIBSSDR 07FDEA05045Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK IS CRACKED/CORRODED, BS 950-950A, RBL 45, WL 208 REMOVED CORRODED SEAT TRACK FROM STA 870 TO 950, 9". FABRICATED NEW SECTION REF BAC DWG 65-19601. TREATED AND PRIMED NEW SECTION. INSTALLED NEW SEAT TRACK. THIS IS CLASSIFIED ASSDR 07FDEA05044Skin · corrodedAFT CARGO COMPARTMENT, BODY STATION 1010 TO 1011, STRINGER 30, WATER LINE 139, BOTH SIDES OF STRINGER, FUSELAGE SKIN CORRODED. REMOVED CORROSION IAW SRM 51-10-6. AFTER CORROSION MATERIAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE ARSDR 07FDEA05041Skin · corrodedEXT FUSELAGE SKIN IS GOUGED AT BS 990, STR S-23L PLUS 6" REMOVED DAMAGE REF SRM 53-30-3 FIG, INSTALLED DOUBLER AND FILLER REF SRM 53-30-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA05040Skin · corrodedLWR FWD CARGO PIT, INNER SKIN IN BILGE HAS PITTING CORROSION UNDER LEVELING COMPOUND, STA 680 PLUS 5, LBL 8". CUT OUT DAMAGE, FABRICATED DOUBLER AND INSTALLED DOUBLER, REF SRM 53-30-3 FIG 1. REPAIR IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA05037Fairing · crackedLT WING FLAP O/B TRACK FAIRING O/B ATTACH FLANGE HAS CRACK JUST AFT OF TRACK AFT MOUNT POINT. REMOVED ATTACHED FLANGE, FABRICATED, LOCATED AND DRILLED NEW ATTACH FLANGE, ALODINED AND PRIMED AND INSTALLED REF SRM 51-30-2, DWG 65-28115, AND SRM 51-10-2 PG 7, SDR 07FDEA05036Pivot · damagedRT AFT PIVOT POINT ON STAB HAS PLAY. REMOVED HORIZONTAL STAB. REPLACED HORIZONTAL STAB HINGE PINS IAW MM 55-10-001-4. REINSTALLED, ADJUSTED & OPS CHECKED HORIZONTAL STAB & ELEVATOR CONTROL SYS. IAW MM 55-10-001-4 & MM 27-30-000-5. STABILIZER HINGE BUSHINGSSDR 07FDEA05035Skin · crackedLEFT WING, INBOARD LEADING EDGE, INNER PANEL AT LEADING EDGE. STATION 106 TO 130 HAS RIVETS PULLED THROUGH AND CRACKS IN SKIN AT 3 LOCATIONS STOP DRILLED CRACKS. HFEC INSP AROUND STOP DRILLED HOLED. FABRICATED REPAIR DOUBLERS, PRIMED AND PAINTED AND INSTSDR 07FDEA05034Skin · crackedLWR FUSE SKIN CRACKED JUST AFT OF TAIL SKID CUT REMOVED DAMAGED SKIN FILLER PLUS DOUBLER, INSTALLED REF SRM 51-10-2 PG2 FOR TREAT AND PRIME REF 53-30-3 FIG 25 FOR REPAIR. THIS IS A CATAGORY "C" REPAIR. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR DHLA200700076Door · lack of lubeFWD ENTRY DOOR WOULD NOT CLOSE ALL THE WAY AND THEN COULD NOT OPEN. FREED FWD ENTRY DOOR. CYCLED DOOR MANY TIMES. DOOR OPERATES NORMALLY PER B727 MM 52-11-22. LUBED DOORS ALL POINTS.SDR 07FDEA04992Support Angle · crackedCABIN UPPER LOBE, STA 1110, AND STR 6R, SIDE WALL SUPPORT ANGLE IS CRACKED IN HALF. REMOVED DAMAGED ANGLE ANGLE REF SRM 51-30-2, FABRICATED REPLACEMENT REF DWG 25FX. TREATED AND PRIMED REF SRM 51-10-02. INSTALLED NEW ANGLE REF SRM 51-30-2. THIS IS CLASSIFSDR 07FDEA04692Frame Splice · crackedFWD LOWER CARGO SPLICE FRAME AT STA 580 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 SPLICE FRAME, FABRICATED AND INSTALLED NEW SPLICE FRAME IAW 727 SRM 51-10-01 AND FEDEX DRG 53FX1370.SDR 07FDEA04686Switch · failedON FLAP RETRACTION TO 2 DEGREES, NR 2 LE FLAP REMAINS EXTENDED. NORMAL HYDRAULICS. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES IAW QRH. NO LUCK. NO ASYMMETRIC CONTROL FORCES NOTED. OBTAINED NORMAL FLAPS 30 LANDING CONFIGURATION. REMOVED AND REPLACED NRSDR 07FDEA04659Skin · gougedRT OVERWING DOOR EXT SKIN IS CORRODED/GOUGED ALONG LWR EDGE. REMOVED CORROSION AND GOUGE REF SRM 51-10-02 AND SRM 52-00-2, CHECKED LIMITS, ORIGINAL "T" IS .045, MATERIAL "T" REMOVED .015" REMAINING "T" IS .030". OUT OF LIMITS VERIFIED BY SRM 52-00-2 PAGE 3SDR 07FDEA04657Floor Support · corrodedSEVERAL LOCATIONS OF CORROSION ON UPPER CHORD FROM FS 760 TO 840, LBL 45.5 REMOVED CORROSION BY REMOVING DAMAGED UPPER CHORD AT STA 760-850, LBL 45.5 REF SRM 51-30-2. REMOVED FLOOR SUPPORT T-CHORD AND ATTACHED FLOOR SUPPORT ASSY'S AT LBL 45.5-62.0 -25.0-45.5 SDR 07FDEA04655Window · corrodedRT WINDOW PLUG AT BS 950 PLUS 10" AND 1020 HAVE CORROSION ON EXT SURFACE. REMOVED AND REPLACED WINDOW PLUGS AT BS 950 PLUS 10" AND 1020 RT SIDE INSTALLED BONDING STRAP (GROUND), PAINTED NEW PLUGS REF MM 56-20-004, SOPM 20-41-02, SWPM 20-20-00 PG4-8. THIS IS SDR 07FDEA04654Floor Support · crackedLOWER FOWARD PIT, STATION 680, FRAME AFT SIDE, RBL 13, BETWEEN STRINGERS 27R AND 28R, FRAME TO FLOOR SUPPORT STRUCTURE ANGLE GOUGE/CRACKED IN RADIUS. REMOVED CRACKED FLOOR SUPPORT CLIP. FABBED NEW CLIP AND DRILLED REF BOEING DWG 65-75172.SDR 07FDEA04653Frame · crackedLOWER STUB FRAME EXTENTION AT BS 560, WEB IS CRACKED ABOVE AND INBD OF STR 21 L, AT RIVET HOLE MARKED END OF DOT WITH BLACK DOT REPLACED LOWER STUB FRAME EXTENSION REF SRM 51-30-2, AND DWG 53FX1350. TREATED AND PRIMED REF SRM 51-10-2.SDR 07FDEA04651Skin · dentedLOWER FORWARD PIT DOOR CUTOUT FORWARD SIDE FUSELAGE SKIN DENTED MEASURE DENT A=2" Y= .073" A/Y= 13.69 DENT WAS OUT OF LIMITS. TRIMMED OUT DENT. REMOVED .310" MATERIAL. REPAIR IS WITHIN LIMITS REF EA 7-5330-113955. USED TOOL IN17-0023 CAL DUE 12-13-08 TO MESDR 07FDEA04650Floorbeam · corrodedSEVERAL LOCATIONS OF CORROSION ON FLOORBEAM FROM FS 760 TO 840, RBL 45.5. REMOVED FLOORBEAM STA 760 - 840, RBL 45.5. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM IAW DWG 65-16279 AND SRM 51-30-02 P1. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA04648Retainer · corrodedRT FWD OVERWING DOOR FRAME, PRESSURE SEAL ATTACH ANGLE IS CRACKED/CORRODED ON ALL FOUR SIDES AS MARKED REMOVED UPPER AND LOWER SEAL ATTACH ANGLES. INSTALLED 2 NEW ANGLE TO DOOR FRAME REF 51-30-02. REPAIR IS CLASSIFIED AS A MINOR.SDR 07FDEA04639Retainer · crackedRIGHT WING LOWER TRAILING EDGE PANEL JUST BELOW NR 11 FLIGHT SPOILER ACTUATOR BULB SEAL RETAINER CRACKED. REPLACED SEAL RETAINER REF 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA04638Skin · corrodedLT 10TH WINDOW PLUG AFT OF AFT OVERWING EXIT HAS CORROSION INSTALLED NEW WINDOW PLUG, PAINTED TO MATCH, REF MM 51-20-013-PG 1-3 AND MM 51-20- 151-7 PAGES 1-3.SDR 07FDEA04637Skin · delaminatedLT OUTBOARD AFT FLAP, T/E INBOARD CORNER IS DELAMINATED REPAIRED LT OUTBOARD AFT FLAP T/E CORNER REF SRM 51-40-20 PARA 6, 7, 19, -21. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA04636Skin · crackedRT MLG GEAR DOOR INSIDE SKIN IS CRACKED REMOVE DAMAGED AREA, INSTALL REPAIR SKIN, DBLR, ACCESS PLATE, REF EO7-5280-7-4301 AND SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA04635Door Frame · corrodedRT FWD OVERWING DOOR FRAME EXTERIOR SURFACE IS CORRODED AT 7:00 POS AS VIEWED FROM OUTSIDE REMOVED CORROSION ON DOOR FRAME REF SRM 51-10-6, MEASURED THICKNESS REF 727 NDT MAN PT 4, 51-00-00, FIG 2 ORIGINAL "T" .063". REMAINING "T" IS .060" IN DEEPEST LOCATIOSDR 07FDEA04634Door Frame · corrodedRT AFT OVERWING DOOR FRAME EXTERIOR SURFACE IS CORRODED ALONG PRESSURE SEAL ATTACH ANGLE AT 5:00 TO 8:00, POS AS VIEWED FROM OUTSIDE. REMOVED CORROSION FROM FRAME SURFACE REF SRM 51-10-1 PG 14-16. MEASURED THICKNESS REF. 727 NDT MAN. PT. 4, 51-00-00. FIG SDR 07FDEA04633Attach Fitting · crackedRT AILERON (OTBD) CAVITY HAS CRACKED ATTACH CLIP LOCATED BET WING TRAILING EDGE RIB AT STA 658.63 AND CAVITY AFT SPAR FABRICATED CLIP BETWEEN WING TRAILING EDGE, STA 658.63 CAVITY AFT SPAR. REF SRM 51-30-02, DWG 65-19289 PG 1. THIS IS CLASSIFIED AS A MINOR RSDR 07FDEA04632Channel · corrodedAFT PIT FLOOR SUPPORT "C" CHANNEL IS CORRODED BS 1165, RBL 7, WL 160. REMOVED DAMAGE IAW SRM 51-10-1 PG 1. FABRICATED REPAIR CHANNEL, AND 2 ANGLES IAW SRM 53-10-5 PG 9/10. INSTALLED REPAIR PARTS IAW 53-10-5, AND 51-30-02 THIS IS CLASSIFIED AS A MINOR REPASDR 07FDEA04631Floor Support · corrodedMAIN CABIN, FS 312 TO 328, LBL 30 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT REF DWG 65-17593 AND SRM SRM 51-30-02 PG 1.SDR 07FDEA04630Frame · corrodedCORROSION ON FWD FRAME AROUND MESC ACCESS DOOR FWD LOCK PIN PLATE, FS 423, BL 0 WL 151. REMOVED CORROSION ON FWD FRAME FOR MESC DOOR, ORIGINAL .040, REMOVED .012", REMAINING .028". LOT OF LIMITS REF SRM 51-10-1 PG 2, NOTE J, AND 53-10-1 PG 2A FIG 1. SHEESDR 07FDEA04629Attach Fitting · cracked5" CRACK ON RT ATTACH FITTING FOR BULKHEAD 1183 BEAM AT BS 1182, BL 0, WL 166 TO 161. REPLACED CHANNEL, REF DWG 69-13353, REF SRM 51-30-2 PG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA04610Skin · corroded13TH LT WINDOW PLUG AFT OF AFT OVERWING EXIT HAS CORROSION ON EXT SURFACE INSTALLED NEW WINDOW PLUG REF MM 56-20-000-4 APPLIED CIC TO INTERIOR REF SRM 51-10-2, PAINTED TO MATCH SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA04609Skin · corroded19TH RT WINDOW PLUG EXTERIOR SURFACE HAS CORROSION (APPROX 720C 6"). REMOVED AND REPLACED WINDOW PLUG REF MM 56-20-000-4, PRIMED AND PAINTED REF SRM 51-10-2 APPLIED LPS REF 51-10-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA04600Stringer · corrodedAFT PIT BILGE STRINGER END FITTING IS CORRODED BS 1178, STR 29L, WL155 (MKD). REMOVED AND REPLACED STR 29L END FITTING PN NR 65-60208-1 IAW 51-30-2. REMOVED CORRODED SECTION OF STR 29L AND REPAIRED STR 29L IAW SRM 53-10-3 FIG I DETAIL I STA 1178-1164. THIS SDR 1014200701Overheat Loop · out of positionAT CRUISE FL 310 AMERIJET FLIGHT 875 NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT WENT OUT AFTER 2 MINUTES AND REMAINED OUT WITH ENGINE AT IDLE ONLY. THE FLIGHT DIVERTED TO KIN. MAINTENANCE DISCOVERED THE STRUT OVERHEAT DETECTOR TOUCHING THE PNEUMATIC DSDR 07FDEA04586Stringer Clip · crackedSTRINGER CLIP CRACKED ON STR 28L, FS 1070. REMOVED STRINGER CLIP REF SRM 51-30-2. FABRICATE NEW STRINGER CLIP 7075-T6 .040 REF BOEING DRW 66-11809-6 PG 1/2. TREATED STRINGER CLIP REF SRM 51-10-2. PRIMED STRINGER CLIP REF SRM 51-10-2. INSTALLED STRINGER CLSDR 07FDEA04585Skin · delaminatedRIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED 72" FROM INBOARD EDGE. REPAIRED SURFACE DELAMINATION REF SRM 51-40-20 PARA'S 7, 14, 15, 19, 20, 22 TAP TEST GOOD. THIS IS CLASSIFIED AS A MAJOR REPAIR. PRIMED AND PAINTED REPAIR AREA REF M/M 51-20-151-7.SDR 07FDEA04552Vane · failedCAPT'S STICK SHAKER WENT OFF. A/C WAS PROPERLY CONFIGURED FOR T/O. PULL C/B. REMOVED AND REPLACED AOA VANE. VANE OPS CKS GOOD, REF B727-200MM, RPT BY: 437820. PERFORMED OPS CK OF EGPWS AND FOUND AOA VANE FAULT FOR LAST FLIGHT LEG. PULLED LEVER LATCH C/B
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