Boeing 727-21C
Service difficulty reports · 217
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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 = '72721C' 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 = '72721C' 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 97FDEA00540Stringer · corrodedCORROSION (C53-224-01,3) ON STRINGER 2 RT FROM BS 950 TO 1010. *S/D* REPAIRED STR 2 RT, BS 950 TO 1010 PER FED-EX SRM 53-10-3 FIG 3.SDR 97FDEA00518Stringer · corrodedCORROSION ON FLANGE OF CROWN STR 3 LT, BS 740 TO 780, 804 TO 827, 846 TO 850. *S/D* REMOVED AND REPLACED STRINGER 3 LT FROM BS 740 TO 870 PER FED SRM 51-10-1, 51-30-02, 51-30-04 AND BAC 5300.SDR 97FDEA00493Chord · corrodedCORROSION (C53-111-01-,2) ON BL 0 CHORD AROUND NUT PLATE HOLES ON O/B FLANGES FROM BS 490 TO 670, LBL 2- RBL 2, WL 20, OUT OF LIMITS PER FED-EX SRM. *S/D* REMOVED DAMAGED CHORD, FABRICATED NEW CHORD AND INSTALLED AT BS 480 TO 700 IAW FED-EX SR-27-53-009.SDR 97FDEA00476Skin · corrodedNR 0872 038 WHILE WORKING NR 0138 FOUND CORROSION ON SKIN AT BS 968 , 995, 1005 - 1010, STR NR 1 RT.SDR 97FDEA00464Skin · corrodedNR 0842 037, STA-PAE, AT BS 520 - 540 BETWEEN STRINGER 3 LT AND 3 RT THE SKIN IS BULGING AT NUMEROUS FASTENER LOCATIONS. ACCOMPLISHED REPAIR PER FED-EX EA NR 7-5330-39818.SDR 97FDEA00462Skin · corrodedNR 0836 034 WHILE WORKING NR 0139 FOUND CORROSION ON SKIN BS 1020 - 1028, STR 2 RT (OUT OF LIMITS). REMOVED CORROSION ON SKIN BS 1020 - 1028, STR 2 RT. FOUND TO BE OUT OF LIMITS IAW FED SRM 53-30-01. REPAIRED SKIN IAW FED SRM 53-30-03 FIG 3.SDR 97FDEA00461Skin · corrodedNR 0826 035 WHILE WORKIG FOUND CORROSION ON SKIN AT BS 990 - 1010, STR 2 RT (OUT OF LIMITS). REMOVED CORROSION ON SKIN AT BS 990 - 1010, STR 2 RT. FOUND TO BE OUT OF LIMITS IAW FED SRM 53-30-01. REPAIRED SKIN IAW FED 53-30-03 FIG 1.SDR 97FDEA00460Floorbeam · corrodedCORROSION ON AND AROUND NUTPLATES ON BS 950 BEAM FROM LBL 62 TO RBL 62, WL 208.1. REPAIRED FLOORBEAM AT BS 950, WL 208, LBL 62 TO RBL 62 IAW FED-EX EA NR 7-5310-34973.SDR 97FDEA00446Frame · crackedWHILE REMOVING 572 FRAME FOUND CRACK AT BS 580, WL 156, RBL 9. REPAIRED PER FEDEX SRM 51-40-3 FIG 1.SDR 97FDEA00444Frame · crackedWHILE REMOVING FLOOR SUPPORT, FOUND CRACK IN FRAME AT BS 500, RBL 9, WL 156 FWD CARGO BAY. *S/D* REMOVED DAMAGE IN FRAME AT BS 500, RBL 9, WL 156 AND REPAIRED FRAME IAW FED-EX SRM 51-40-3.SDR 97FDEA00440Intercostal · corrodedCORROSION (C53-111-01-,2) UNDER END GROUND NUT PLATES ON FRAME BS 700 BETWEEN 27R AND 27L (FWD BAY). *S/D* REMOVED CORROSION FROM UNDER END GROUND NUT PLATES ON FRAME BS 700 BETWEEN STR 27R AND 27L (FWD BAY) FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. SDR 97FDEA00439Frame · corrodedCORROSION (C53-111-01) ON FRAME BS 500, STR 26L. * S/D* REMOVED CORROSION ON FRAME BS 500, STR 26L. FRAME OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED FRAME PER FED-EX SRM 51-40-3.SDR 97FDEA00424Floorbeam · corrodedNR 0399 024 CORROSION (C53-224-01(3)) ON BS 1030 BEAM FROM LBL 47 TO RBL 62, WL 208.1. CORROSION ON BS 1030 BEAM FROM LBL 47 TO RBL 62, WL 208.1 WAS BLENDED AWAY. DAMAGE AT BS 1030, RBL 47 - 60 FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED DAMASDR 97FDEA00426Clip · crackedCRACKED STRINGER CLIP BS 990, STRINGER 5 LT. *S/D* REMOVED AND REPLACED WITH NEW CLIP AT BS 990, STR 5 LT IAW FED-EX SRM 51-10-1.SDR 97FDEA00423Chord · corrodedCORROSION (C53-111-01, 2) ON BL 0 CHORD AROUND NUT PLATE HOLES ON O/B FLANGES FROM BS 490 TO 670, LBL 2 TO RBL 2, WL 200 (OUT OF LIMITS PER FED-EX SRM). *S/D* REMOVED AND REPLACED CORRODED BL 0 CHORD FROM 460 TO 740, LBL 2 TO RBL 2, WL 200 WITH A NEW CHORD. SDR 97FDEA00422Bulkhead Web · corrodedCORROSION (C57-174-01) ON BS 870 BULKHEAD WEB RBL 70-LBL 70, WL 176 TO 138. *S/D* REMOVED CORRODED WEB BS 870, RBL 70, WL 176 TO 138 AND INSTALLED NEW WEB IAW FED-EX EA 7-5710-36189A.SDR 97FDEA00418Spar Chord · corrodedNR 0735 025 - STA-PAE - CORROSION (C57-174-01) BS 870 REAR SPAR LOWER CHORD RBL 10-15, LBL 20-30, WL 138. REMOVED CORROSION ON LOWER CHORD BS 870 FOUND LOWER CHORD TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED REAR SPAR LOWER CHORD PER FEDSDR 97FDEA00417Spar Chord · corrodedCORROSION (C57-174-01) BS 870 REAR SPAR UPPER CHORD, RBL 30 TO 50, LBL 20 TO 40, WL 178. *S/D* BLENDED REMOVED CORROSION ON BS 870 REAR SPAR UPPER CHORD FOUND TO BE OUT OF LIMITS PER FED-EX 727 SRM 53-10-1. REMOVED AND REPLACED CHORD PER FED-EX EA 7-5710-36SDR 97FDEA00389Chord · crackedCRACK IN RT MID NOSE CHORD BS 302 TO BS 294.5, RBL 16, WL 169. *S/D* REMOVED AND REPLACED RT MID NOSE CHORD BS 294.5 TO BS 350, RBL 16, WL 169 IAW FED-EX DR6 65-18415.SDR 97FDEA00388Strin Ger · corrodedNR 0413 006, CORROSION (C53-224-02) ON LT STRINGER 7, BS 381 TO BS 393. *S/D* REMOVED AND REPLACED STRINGER 7 LT, BS 360 TO 410 PER FED-EX SRM 53-10-3.SDR 97FDEA00387Frame · corrodedCORROSION (C53-111-01) ON FRAME AT BS 560, STR 26L. *S/D* REMOVED CORROSION ON FRAME AT BS 560, STR 26L. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED DAMAGED AREA PER FED-EX SRM 51-40-3. REPAIRED PER FED-EX SRM 51-40-3. ALODINED AND PRIMED PSDR 97FDEA00391Floorbeam · corrodedCORROSION ON BS 1110 FLOORBEAM FROM BL 0 AND RBL 62, WL 208.1. *S/D* CORROSION ON BS 1110 BEAM FROM BL 0 TO RBL 62, WL 208.1 WAS FOUND TO BE OUT OF LIMITS AT BS 1110, RBL 35 TO RBL 70 PER FED-EX SRM 53-10-1. REPAIRED DAMAGED SECTION OF FLOORBEAM PER FED-EX SDR 97FDEA00390Floorbeam · corrodedCORROSION (C53-221-01) ON FLOORBEAM UNDER NUT PLATE, STA 277, RBL 16.5, WL 207.9. *S/D* REPAIRED DAMAGED FLOORBEAM BS 277, RBL 16.5, WL 207.9 IAW FED-EX SRM 51-40-4.SDR 97FDEA00396Beam · crackedFWD CARGO DOOR NR 4 TRANSVERSE BEAM HAS TWO CRACKS IN O/B RADIUS. *S/D* REMOVED AND REPLACED FWD CARGO DOOR NR 4 TRANSVERSE BEAM IAW FED SRM 51-30-2.SDR 97FDEA00392Clip · crackedNR 0189 001 CRACKED STRINGER CLIP AT BS 1010, STRINGER 6 R/H. REMOVED AND REPLACED STRINGER CLIP AT BS 1010, STRINGER NR 6 R/H. IAW FED-EX SRM 51-30-2.SDR 97FDEA00072Warning Switch · stuckAIR CONDITIONER WOULD NOT PRESSURIZE AFTER TAKEOFF. AIR TURNBACK. FOUND AFT CARGO DOOR OPEN AND DOOR WARNING SWITCH STUCK. FREED SWITCH, CLOSED DOOR AND OPS CK GOOD.SDR 96ZZZM1387Duct · crackedDURING CLIMB-OUT FROM TOLEDO, NR 2 ENGINE FIRE WARNING SOUNDED. CREW FIRED ONE EXTINGUISHER AND SHUT DOWN THE ENGINE. AIRCRAFT LANDED UNEVENTFULLY AT TOL. MAINTENANCE DISCOVERED 13TH STAGE BLEED SADDLE DUCT CAP (RT) FAILED AT WELD ALLOWING HOT BLEED AIR INTOSDR UPS205333Mid Spar · chafedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRED PER UPS EO 727-55-0309.SDR UPS205319Wedge · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, REMOVED AND REPLACED RT I/B MIDFLAP T/E WEDGE. REPLACED AS REQUIRED PER SRM 51-30-2.SDR UPS205332Rib · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT NR 2 ELEVATOR HINGE SUPPORT RIB IS CRACKED ON I/B UPPER FLANGE NEAR AFT END. REMOVED RT NR 2 ELEVATOR HINGE SUPPORT RIB IAW SRM 51-30-2.SDR UPS205331Slat · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IAW MM 27-81-11.SDR UPS205330Bonding Jumper · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00.SDR UPS205329Angle · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51-30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1.SDR UPS205327Rod End · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILERON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00.SDR UPS205326Hinge Tab · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B AILERON TAB HINGES ARE CORRODED. REMOVED AND REPLACED RT WING I/B AILERON TAB HINGES IAW SRM 51-30-02 AND MM 51-10-0.SDR UPS205328Hinge Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND REPLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-SDR UPS205325Hinge Arm · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE ARM IS CORRODED AROUND BOLT HOLE. REMOVED AND REPLACED HINGE ARM IAW MM 27-10-01 AND 27-10-0.SDR UPS205324Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON TAB HINGE FITTINGS CORRODED, 3 EA. REMOVED AND REPLACED LT AILERON TAB FITTINGS IAW SRM 51-30-2 AND MM 27-10-0.SDR UPS205323Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT FITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443.SDR UPS205322Fitting · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT FITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443.SDR UPS205321Mid Spar · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR UPPER INTERIOR SURFACE AFT SIDE 49 AND 55 I/B OF THE O/B END OF MID SPAR. REPLACED ON NRC 368443.SDR UPS205320Mid Spar · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR AFT SIDE 54 AND 58 O/B OF THE I/B END OF MID SPAR. REPLACED ON NRC 368443.SDR UPS205300Intercostal · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 682, RBL 10 - LBL 10, WL 152. REPLACED STRUCTURE LBL 10 - RBL 10, STA 682, WL 152 I/A/W SRM 51-29-1.SDR UPS404656Switch · out of adjustDURING CLIMBOUT, THE RT MAIN GEAR DOOR ANNUNCIATOR LIGHT ILLUMINATED, AFTER POSITIONING THE GEAR HANDLE TO THE OFF POSITION. MAINTENANCE CYCLED THE LANDING GEAR AND THE RT MAIN LIGHT ILLUMINATED AGAIN WITH THE GEAR. ADJUSTED AND TESTED DOOR SWITCH PER MM 32-SDR 95FDEA01159Retract Mech · lack of lubeCDG - UPON GEAR EXTENTION LT AND RT MAIN GEAR INDICATED DOWN AND LOCKED WITH GREEN LIGHTS, NOSE GEAR RED LIGHT ILLUMINATED, DID NOT HEAR ANY INDICATION THAT NOSE WHEEL EXTENDED. LUBRICATED NOSE GEAR ASSY PER MM 12-21-11, PERFORMED TEST NOTE GEAR RETRACTION ANSDR 95FDEA01073Hyd Lines · failedA-SYS FAILURE UPON GEAR RETRACTION, QTY ZERO, PRESS ZERO, RED PAGE COMPLIED WITH. APPROXIMATELY 5 MINS FLT TIME WITH FLUID SHUTOFF, PUMPS ON, 9 MINS WITH THEM OFF. HYDRAULIC PUMPS RAN 1 MIN PRIOR TO TURNING THEM OFF. FOUND HOLE IN RETRACT LINE IN NOSE GEAR.SDR UPS23508Hyd Fluid · leakingBEGINNING OF DESCENT INTO SDF, AS THRUST LEVERS WERE BROUGHT TO IDLE THE SYSTEM 'B' HYDRAULIC LIGHTS ON F/O PANEL ILLUMINATED. BOTH SYSTEM 'B' PUMP LOW PRESS LIGHTS ON F/O PANEL ILLUMINATED AND SYSTEM QUANTITY DROPPED TO 0. LOSS OF SYSTEM 'B' CHECKLIST WAS ASDR UPS203508Hyd Pump · malfunctioned(SUPPLEMENTAL MRR) PILOT REPORTED THAT AT BEGINNING OF DESCENT WHEN THRUST LEVERS WERE BROUGHT TO IDLE, THE SYSTEM 'B' HYDRAULIC LIGHTS ON F/O PANEL ILLUMINATED. BOTH SYS 'B' PUMP LOW PRESS LIGHTS ON F/O PANEL ILLUMINATED AND SYSTEM QUANTITY DROPPED TO ZERO. SDR 95FDEA00500Door Frame · crackedAFT ENTRY DOOR L/T SIDE FRAME PREVIOUS REPAIRED CRACK ISN'T CONTAINED AT STOP DRILL (2 PLACES). REMOVED DAMAGED AREA FROM WL 218 TO 239, FABRICATED AND INSTALLED NEW SEGMENT OF FRAME AND SPLICE DOUBLERS PER FED EX SRM 51-40-3.SDR 95FDEA00499Bonding Strap · corrodedNR 1 K-FLAP O/B LOWER BONDING VAMPER UPPER ATTACH POINT IS CORRODED. CLEANED AND TREATED PER EWO NR 95-2426, CORROSION ON NR 1K-FLAP O/B LOWER BONDING VAMPER ATTACH POINT AS WELL AS FEDEX EA 7-5750-24438.
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