Boeing 727-233
Service difficulty reports · 3,034
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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"
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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 CA080801003Engine · power loss(CAN) WHILE AIRCRAFT WAS IN CRUISE ENROUTE, THE ACFT EXPERIENCED AN UNCOMMANDED POWER LOSS, DECELERATING TO FLIGHT IDLE. THE CREW SELECTED NR 2 THRUST TO IDLE AND THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. THE ACFT FERRIED FOR SDR 08FDEA03050Sensor · failedLANDING LEVER HANDLE FAILED TO MOVE PAST THE OFF POSITION. FOLLOWED QRH PROCEDURES AND IT FAILED TEST NR 1. REINSTALLED GROUND SENSE LOWER LINK TO SCISSORS LT GEAR, PER SMP AND SAFETIED BOLT. REMOVED AND REPLACED AIR SAFETY SENSOR IAW M/M 32-09-221-4. PESDR 08FDEA03042Channel · corrodedLOWER FUSE WING BODY FILLET FRG SUPPORT FRAME U CHANNEL IS CORRODED BS 773, LBL 9 - RBL 9, WL 140. REMOVED U CHANNEL REF SRM 51-30-2. FABRICATED "U" CHANNEL ON SHOP SNRM NR N00692, DRILLED UP, TREATED, PRIMED AND PAINTED "U" CHANNEL REF DWR 65-58504, SRM 51SDR 08FDEA03038Skin · delaminatedDELAM SPOTS TOP NR 2 SPOILER REMOVED DAMAGE AREAS, CLEANED AND PREP IAW B727 SRM 51-40-20 PG 12-14,42-47. FABRICATED REPAIR FILLERS (2) APPROX 7 BY 5, 22 BY 3 AND REPAIR DOUBLERS (2) APPROX 10 BY 6.5 AND 25 BY 4.5 USING .025 7075 T6 IAW B727 SRM 51-40-20 PG SDR 08FDEA03019Landing Gear · malfunctionedON DEPARTURE, LANDING GEAR FAILED TO RETACT. COULD NOT RAISE HANDLE PAST OFF. PULLED LATCH AND AURAL C/B'S, STILL COULD NOT RAISE HANDLE PAST OFF POSITION. SYSTEM FAILED EXTENSION TEST, PER RED TABS DID NOT ATTEMPT TO USE LEVER LATCH TRIGGER.SDR 08FDEA02994Intercostal · corrodedDELTA BEAM AT STA 740 HAS CORROSION AROUND AND UNDER HEADS OF SEVERAL FASTENERS. CAN BE SEEN THRU ACCESS HOLE BELOW BEAM. REMOVED CORROSION. ORIGINAL "T" .107 LOSS AT LOWEST POINT IS .028 REMAINING "T" IS .079. OUT OF LIMITS REF SRM 53-10-1 FIG 101 DETAISDR 08FDEA02985Bracket · crackedNR 1 ENG UPPER COWL, BRACKET CRACKED AT FWD O/B LOWER CORNER REMOVED AND REPLACED CRACKED SEGMENT, PAINTED AFFECTED AREA OF COWLING. REF SRM 51-30-2 PG 2, MM 51-20-151-7 PG1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02984Fairing · crackedRT BODY FAIRING PANEL NR 3349 CRACKED AT EDGE. REMOVED DAMAGED EDGE PLATE. VERIFIED MATERIAL FOR NEW EDGE PLATE, FABRICATED NEW EDGE PLATE, TREATED AND PRIMED AND INSTALLED. REF DWR 65-58505 AND SRM 51-10- 2 PG1, 51-30-2 PG1. THIS IS CLASSIFIED AS A MINORSDR 08FDEA02983Retainer · corrodedLEFT MLG W/W LOWER FWD WING PANEL HAS CORROSION ON SEAL RETAINER STRIP NEAR LOWER MLG SUPPORT BEAM, WSS 217. REMOVED AND REPLACED LEFT MLG W/W LOWER FWD WING PANEL SEAL RETAINER AT WSS 217 REF SRM 51-30-2 PG 2 AND DWR 65-21656. THIS IS CLASSIFIED AS A MINOR SDR 08FDEA02958Bulkhead · corrodedCORROSION AT BS 1166 BULKHEAD RT SIDE "T" ANGLE (AT BOTTOM NUTPLATE AFT SIDE OF BULKHEAD). REPLACED T-CHORD AT AFT PIT BULKHEAD BS 1166 RBL 25 INCHES. REMOVED CORROSION AND FOUND NOT WITHIN ALLOWABLE LIMITS ORIG MATERIAL THICKNESS IS .063, MATERIAL LOSS IS .SDR 08FDEA02954Floor Support · corrodedUNDER FWD LAV STA 328 TO 344 FLOOR SUPPORT RBL 52 HAS CORROSION AROUND NUTPLATES REMOVED AND REPLACED SUPPORT FROM STA 326-344 RBL REF SRM 51-30-2 PG 2, FLOOR SUPPORT AT RBL 52 STA 328-344. FOUND TO BE WITHIN LIMITS OF SRM 53-10-06, TREATED AND PRIMED REF SRMSDR 08FDEA02926Floor Support · corrodedFLOORBOARD, FWD LAV SUPPORT NUT PLATES RUSTED STA 305 - RBL 44. REMOVED FLOOR SUPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIG. MATERIAL THICKNESS .040 INCH. REMAINING .031 INCH REMOVED .009'. FABRICATED NEW ANGLE, PENATRANT INSP FOR CRACSDR 08FDEA02923Module · failedDURING GEAR EXTENSION RECEIVED UNSAFE NOSEGEAR (NO GREEN LIGHT) ALL GEAR INDICATIONS S/O PANEL NORMAL, NO GEAR WARNING HORN DURING THROTTLE REDUCTION. COMPLIED WITH QRH, MANUAL GEAR EXTENDED. LIGHT REMAINED OUT. AFTER CRANKING NOSEWHEEL TO STOPS, LIGHT REMASDR 08FDEA02945Panel · delaminatedUPPER TAIL PANEL NR 9607, INNER FOIL DISBONDED REPAIRED TEDLAR COVERING ON INNER SURFACE REF SRM 51-40-9 STEP 11 PG 18. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02939Panel · crackedPANEL 3617 BOTTOM AFT END CRACKED REPAIRED PANEL 3617 REF SRM 51-40-9 STEPS 3D, 4E, 4F, PGS 3-7 AND AMM 51-20-051 PG1, AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02938Panel · delaminatedNR 3 SLAT UNDERWING PANEL NR 6224 HAS AREA OF DELAMINATION REPAIRED PANEL 6224 REF SRM 51-40-9 STEPS 3D, 4E, 4F PG3-7 AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02927Door · gougedMAIN CARGO DOOR, AFT EDGE LOWER CORNER GOUGED LOWER AFT CORNER GOUGED BEYOND LIMIT. REMOVED DOUBLER FABRICATED NEW DOUBLER, TREATED AND PRIMED. INSTALLED NEW DOUBLER REF 727 P-FSRM 52-30-2 PG 1/2. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02925Frame · corrodedRT AFT EMERGENCY EXIT HATCH LOWER FRAME OUTER SURFACE HAS CORROSION. REMOVED CORROSION REF SRM 52-00-2 NDT THICKNESS ORIGINAL "T" .063, .005 LOSS, .058, DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED PRIMED AND PAINTED REWORKED AREAS REF SDR 08FDEA02924Frame · corrodedRIGHT FWD EMERGENCY HATCH FRAME LOWER OUTER SURFACE CORRODED BETWEEN SEAL RETAINER AND SKIN REMOVED CORROSION REF SRM 52-00-2. NDT THICKNESS ORIG "T" .063 LOSS .005 .058. REMAINING DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED, PRIMED ASDR 08FDEA02922Skin · crackedLEFT WING INBD AFT FLAP, 3RD ATTACH FITTING OUTBD SKIN CRACKED FABRICATED REPAIR PARTS AT LEFT WING T/E AFT FLAP, THIRD ATTACH FITTING O/B SKIN, REF 27-50-4 FIG 11. TREATED, PRIMED AND INSTALLED, REF SRM 51-20-2 PG 1-7, 57-50-04 FIG 11, 51-30-2 PG 2-4. PAISDR 08FDEA02921Floor Support · corrodedFLOORBOARD SUPPORT NUTPLATES RUSTED STA 305-312 RBL 55 FWD LAV. REMOVED FLOOR SUPPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORIG MATERIAL THICKNESS .040, REMAINING .033, REMOVED .007. INSTALLED NEW ANGLE REF SRM 51-30-2 PG 2, SRM 53-10-1 PG 1SDR 08FDEA02917Skin · corrodedC1 PIT BILGE AREA-STR 28R STA 680 LEVELING COMPOUND BULGING WITH CORROSION ON SKIN. REMOVED DAMAGED COMPOUND. FOUND CORROSION AT SKIN AND NDT FOR LIMITS ORIGINAL "T" .070 LOSS AT LOWEST POINT IS .034, REMAINING T IS .036 IS OUT OF LIMITS REF SRM 53-30-3. RESDR 08FDEA02916Floor Panel · corrodedMAIN DECK LAV FLOOR WEB PANEL, UPPER LWR SURFACES ARE CORRODED BS 304 - 340, RBL 40 - 60, WL 208. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .042 INCH, REMAINING .035', REMOVED .007. FOUND TO BE OUT OF LIMITS REF DRM 53-10-1 PG 2, TOOL ID AAR 9800 CAL DSDR 08FDEA02915Floor Support · corrodedFWD LAV FLOOR SUPPORT STA 305-312 RBL 42 NUTPLATES RUSTED AND FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM, ORIGINAL THICKNESS .070, REMAINING .066. REMOVED .004, FOUND TO BE WITHIN LIMITS, REMOVED CORROSION FROM FLOOR SUPPORT, ORIG THICKNESS.070, SDR 08FDEA02913Channel · crackedE/E DOOR CUT-OUT FWD ANGLE CRACKED BY LATCH REPLACED CUT OUT FWD ANGLE AND RIGGED E/E DOOR REF BOEING DWR 65-16351, SRM 51-30-01 PG 1-10, SRM 51-30-5 PG 3, SRM 51-30-2 PG 2/3, AMM 51-20-151 PG 1-6, AMM 20-60-001 PG10, MM 52-40-011 PG 1. THIS IS CLASSIFIED AS SDR FDEA200807152876Switch · malfunctionedDURING NORMAL LANDING GEAR EXTENSION, RECEIVED UNSAFE NLG INDICATION. C/W QRH, LIGHT TEST OK, USED MANUAL NLG GEAR EXT AND RECEIVED SAFE NLG IND AFTER ONLY .2500 TURN OF HAND CRANK. SWUNG NOSE GEAR SEVERAL TIMES IAW MM. REMOVED AND REPLACED NLG LOCK AND POSSDR 08FDEA02883Skin · damagedGOUGE IN SKIN AT FUSELAGE STA 265 FWD OF ELEC POWER RECEPTACLE ACCESS DOOR TRIMMED OUT DAMAGE SKIN (DIM 4 BY 1 1/4) IAW EA 7-5330-122320. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 16 AND 2. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW SSDR 08FDEA02885Skin · damagedLT WING T/E O/B FOREFLAP HAS DEEP GOUGE ON UPPER SURFACE AT WS 450. REMOVED DAMAGED AREA IAW B727 SRM 51-40-20 PARAGRAPH 12 AND FABRICATED FILLER AND DOUBLER FROM 2024T3 .016 (3 BY 3) AREA IAW B727 SRM 51-40-20 GAUGE 59. BONDED FILLER AND DOUBLER, SEALED EDGSDR 08FDEA02884Skin · gougedFUSELAGE EXTERIOR SKIN GOUGED STA 1090 STR 22R. BLENDED OUT DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-30-1 FIG 1 AND 2. REPAIRED SKIN FUSELAGE STA 1090 STRINGER 22R IAW EA 7-5330-122334.SDR 08FDEA02876Switch · malfunctionedDURING NORMAL LANDING GEAR EXTENSION RECEIVED UNSAFE NLG INDICATION. C/W QRH, LIGHT TEST OK, USED MANUAL NLG GEAR EXT AND RECEIVED SAFE NLG IND AFTER ONLY 1/4 TURN OF HAND CRANK. SWUNG NOSE GEAR SEVERAL TIMES PER 727-200 MM 07-11-000-2 CND. REMOVED AND REPLSDR 08FDEA02841Angle · corrodedBS 740 BULKHEAD LOWER FWD SURFACE, ANGLE LBL 4.5 TO RBL 4.5, WL 146.5 HAS CORROSION ON AFT SURFACE FABRICATED NEW ANGLE REF SRM 51-10-2 PG 2, DWR 65-23555. TREATED AND PRIMED REF 51-10-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02834Fitting · corrodedBS 740 BULKHEAD LOWER SURFACE, "T" ANGLE AT RBL 5" WL 146.5 CONNECTION TO DELTA BEAM "T" FLANGE IS CORRODED NEW T ANGLE FABRICATED ON SHOP NON-ROUTINE N00670. REMOVAL AND INSTALLATION ACCOMPLISHED ON N00167. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02796Structure · crackedNUMBER 3 CARGO DOOR LOWER FWD "T" CHORD CRACKED AT FASTENERS REPAIRED LOWER FWD "T" CHORD. REMOVED LWR INNER DOOR SKIN REF SRM 51-30-2. FABRICATED REPAIR ANGLES AND FILLER REF SRM 51-40-04 PG 14-16 FIG 3. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-44-04 PGSDR 08FDEA02780Support Bracket · corrodedCORROSION AROUND BOLT HOLE AT STA 340 FITTING SUPPORT BRACKET JUST BEHIND NOSE WHEEL WELL LT SIDE. REMOVED FITTING SUPPORT AT STA 340 AFT OF NOSE WHEEL WELL LT SIDE. TREATED AND PRIMED NEW SUPPORT FITTING REF SRM 51-30-2 PG 1-20 AND MM 51-20-7. THIS IS CLASSDR 08FDEA02778Retainer · corrodedRT WING REAR SPAR LWR CHORD, APPROX 12" IB OF FWD MLG TRUNNION, SEAL RETAINER CORRODED AT OB END. REMOVED FAIRING AND SEAL RETAINER REF SRM PG 2 LOCATED AND DRILLED NEW SEAL RETAINER REF SRM 51-30-5 PG 1, INSTALLED SEAL RETAINER AND FAIRING REF SRM 51-30-2SDR 08FDEA02777Frame · corrodedLWR AFT CARGO PIT, CORROSION ON UPPER FLANGE OF FRAME AT STA 1090 STR 27L REMOVED CORROSION, ORIGINAL "T" .063, REMOVED .017, REMAINING .046 OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM 7075-0 .063, HEAT TREAT T6, APPLIED ALODINE, PRIMER AND INSTALLED REPAISDR 08FDEA02761Skin · dentedFUSELAGE, C-3 DOOR HAS NUMEROUS DENTS AND BULGES ON EXTERIOR SKIN OF DOOR REMOVED C-3 DOOR ASSY AND HANDLE IAW MM 52-35-051-4 AND SRM 51-30-2. REMOVED, FABRICATED AND INSTALLED NEW C-3 DOOR SKIN IAW EA 7-5230-22339. REINSTALLED C-3 DOOR HANDLE AND ATTACHED PSDR 08FDEA02760Skin · damagedLWR FUSELAGE, DRAIN HOLE DAMAGED AT STA. 355 STR 30. REMOVED SKIN PANEL IAW B727 SRM 51-30-2. FABRICATED NEW SKIN MAT USED 2024T3 .050 (27 BY 8.75) IAW B727 SRM 53-30-2 FIG 2 AND 51-30-5. TREATED AND PRIMED NEW SKIN AREA IAW B727 SRM 51-10-2. INSTALLED NEWSDR 08FDEA02739Slat · crackedLT WING NR 4 SLAT FENCE UPPER AFT END COMPOSITE IS CRACKED AND DELAMED. REPAIRED NR 4 SLAT FENCE REF SRM 51-40-9 STEP 7 PG 9 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02258Actuator · out of adjustTEST FLIGHT, RMG SHOWED UNSAFE IND ON THIRD EXTENSION. NO GREEN DOWN AND LOCKED LIGHT, RED DOOR OPEN LIGHT ON. VISUAL INSPECTION BY TOWER AND OTHER A/C CONFIRMED RIGHT MAIN GEAR WAS STILL UP. CYCLED IAW RED TABS AND GOT SAFE DOWN AND LOCKED INDICATION. ADJSDR 08FDEA02190Duct · leakingAFTER TAKEOFF IN CLIMB-OUT NR 3 ENG STRUT OVERHEAT ILLUM. RAN QRH WHICH DETERMINED POSSIBLE LEAK ON FUSELAGE SIDE. WITH LIGHT EXTINGUSHED CONT CLIMB AND CABIN PRESSURE WOULD NOT HOLD AT FL 320 WITH ONE PACK OPERATION. REQ DESCENT TO 10,000 FT TO CONTROL CABSDR 08FDEA02169Hydraulic System · malfunctionedDURING DESCENT LOST ALL OF SYS A HYD QUANITY PRESSURE WAS NORMAL - 3000 PSI AND NO A.R.E. OR ENG PUMP LOW PRESSURE LIGHTS WERE ILLUMINATED AFTER TEN MINUTES BOTH ENG 1 AND ENG 2 LOW PRESSURE LIGHTS STARTED TO FLASH. TURNED BOTH SYSTEM OFF AT THE PUMP SWITCSDR 08FDEA02134Angle · crackedRT WING INBOARD MID FLAP LOWER AFT CHORD ANGLE IS CRACKED AT WBL 110. CUT OUT DAMAGED SECTION DIM 47 1/4 INCH IAW B727 SRM 51-10-1, FABRICATED FILLER REPAIR USING BAC1503-100046 7075-T6 PO NR 8177105 DIM 47 1/4 INCH BY 2 INCH AND SPLICE USING BAC1503-100046 7SDR 08FDEA02133Beam · corrodedKEEL BEAM END TOP ATTACH ANGLE ON BACK OF BULKHEAD AT FS 740 HAS CORROSION ON TOP SIDE OF ANGLE AT RBL 4, ABOVE CONTROL CABLE PULLEY WHEELS. REMOVED AND REPLACED ANGLE REF SRM 51-30-02. FABRICATED REPLACEMENT ANGLE ON N/R N00726. FLAP PEENED, ALODINED, PRISDR 08FDEA02132Beam · corrodedDELTA BEAM INTERIOR RT LOWER CHORD AT BS 747 - 749, RBL 5, IS CORRODED ON INNER SURFACE AT AND AROUND SPLICE. BLENDED CORROSION AT LOWER, FWD CHORD. FOUND TO BE OUT OF LIMITS, REF DWG 69-47111. REPLACED CHORD REF DWG 65-47111. THIS IS CLASSIFIED AS A MAJORSDR 08FDEA02129Beam · corrodedCORROSION INSIDE DELTA BEAM STA740, LBL 3, WL 148 CUT AWAY LWR WEB SECTION OF DELTA BOX TO FOM. REMOVED CORROSION FROM DELTA BEAM STA 740, LBL 3, WL 148. VERIFIED MATERIAL LOSS BY NDT, AND FOUND TO BE OUT OF LIMITS REF DWG 65-23555. REPLACED INTERCOSTAL REFSDR 08FDEA02127Frame · corrodedCORROSION ON TOP OF WING TO BODY FAIRING FRAME WORK AT TWO FWD ADF ANTENNA LEAD POSITION CLAMP ATTACH AT FS 730F, RBL 10, INBOARD OF RT RAM AIR DUCT REMOVED PANELS REF SRM 51-30-2, REMOVED CORROSION REF SRM 53-10-01. FOUND TO BE OUT OF LIMITS REF SRM 51-20-01SDR 08FDEA02074Bulkhead · corrodedFWD PANEL RACK: BULKHEAD BS 720 FWD PIT FRAME CORROSION AROUND NUT PLATES (MKD) FABRICATED NEW FRAME ANGLE REF DAD DWG 65-82623. TREATED PRIMED RES AMM 51-20-021-7 PG 1-7 51-20-031-7 PG 1-7. MARKED PART REF FEDEX GMM 7-0-1001. THIS IS CLASSIFIED AS AMINOR RSDR 08FDEA02073Beam · corrodedRT A/C EQUIP BAY PANEL 3455 HAS CORROSION UNDER FWD HINGE PLATE ON FRAME REMOVED PNL NR 3453, 3358, 3465. SPLICED IN NEW BEAM ASSY P/N NR 65-58502-90. FABRICATED 4. REPAIR ANGLES, TREATED AND PRIMED AND INSTALLED. RE-INSTALLED A/C PANELS. REF SRM 51-30-0SDR 08FDEA02072Mount · corrodedCORROSION ON CARGO TIE DOWN MOUNT ON BOTTOM INBOARD FWD CORNER AT FS 720, LBL 22, WL 156. REMOVED AND REPLACED DAMAGED FITTING, REF SRM 51-30-02 PG 1-3. FITTING FOUND TO BE OUT F LIMITS, REF BOEING DWG 65-57848 ITEM NR 1, ORIG THK IS .110 INCH, MAT LOSS IS
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