Boeing 727-22
Service difficulty reports · 1,282
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 = '72722' 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 = '72722' 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 01FDEA00874Warning Light · illuminatedNR 3 ENG BLEED AIR TRIP LIGHT ILLUMINATED AND WOULD NOT RESET. *S/D* COMINGSDR 01FDEA00859Skin · crackedN 457 RIGHT OUTBOARD AILERON TAB LEAD EDGE CRACKED. R/R TAB PER MM 27-10-041-4.SDR 01FDEA00858Battery · dischargedFWD ENTRY DOOR ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY ASSY PER MM 33-50-121-2.SDR 01FDEA00857Skin · crackedN 418 EXTERIOR SKIN CRACKED AT LWR HINGE CUTOUT. R/R SKIN PER SRM 52-00-03.SDR DHL2001707013Switch · inoperativeNOSE GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION, LIGHT TEST OK. REMOVED NLG POSITION SWITCH AND LINKAGE PER M/M 32-61-71. INSTALLED NLG POSITION SWITCH IAW B727 MM 32-61-71. OPS CHECK GOOD.SDR CA011012013Frame · cracked(CAN) APPROXIMATELY 1 INCH CRACK AT FORWARD CARGO PIT DOOR CUTOUT FRAME LOCATED BS 540 BETWEEN S20 AND S21R AT DOOR STOP.SDR DHL2001707012Battery · dischargedEMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-71.SDR 01FDEA00835Actuator · failedLEADING EDGE FLAP LIGHT CAME ON AT 10L FT WITH FLAPS UP. REMOVED AND REPLACED NR 2 & 6 SLAT ACTUATORS PER MM 27-81-032-4.SDR CA011012012Rib · cracked(CAN) DURING C-CHECK INSPECTION FOUND RT WING RIB CRACKED APPROXIMATELY 1.25 INCH, LOCATION AT WS 519 STR 6 LOWER FLANGE ATTACH POINT.SDR DHL2001707011Bulkhead · crackedON DROP IN CHECK, FWD CARGO COMPT, WING CENTER SECTION FWD BULKHEAD WEB CRACKED (APPROX 1 INCH) RBL 29 APPROX 14 INCHES ABOVE PRESS SPAL BETWEEN VERTICAL ROW OF FASTENERS. STOP DRILLED CRACK 2 PLACES IN FWD CARGO COMPL, WING CENTER SECTION FWD BULKHEAD WEB ATSDR CA011012011Skin · cracked(CAN) 0.50 INCH CRACK FOUND IN RT ELEVATOR LOWER INBOARD SKIN.SDR CA011012010Frame · cracked(CAN) DURING INSPECTION, A CRACK WAS FOUND AT A TOOLING HOLE IN THE BS 632 FRAME ABOVE STRINGER 11 RT. CRACK LENGTH 0.50 INCH ON ONE SIDE OF TOOLING HOLE, OTHER SIDE 0.38 INCH IN LENGTH.SDR CA010907006Nut · split(CAN) ON RT MAIN LANDING GEAR FOUND TRUNNION NUT SPLIT ON ONE SIDE, ON THE RT SUPPORT ASSEMBLY TRUNNION.SDR DHL2001707010Switch · malfunctionedNR 2 ENGINE OIL PRESSURE LIGHT CAME ON DIM DURING FLIGHT. COULD EXTINGUISH LIGHT BY RETARDING THRUST TO IDLE INITIALLY. BUT EVENTUALLY CAME ON AT IDLE. OIL TEMP READING 135. QUANTITY DECREASED FROM 4.2 GAL AT T/O. R&R MAIN OIL FILTER, FOUND SOME CARBON BB'S NOSDR DHL2001707009Bleed Valve · failedT/O THRUST LEFT MANIFOLD DUCT PRESSURE ROSE TO 100PSI DEFERRED PER MAINT. CONTROL 36-11-1 MB. WHEN ATTEMPTING TO START ENGINES TO CHECK PRESSURIZATION, NR 1 ENG WOULD NOT START. NO DUCT PRESSURE DROP AND START VALVE OPEN LIGHT DID NOT ILLUMINATE. RESET C/B- SDR 01FDEA00673Bracket · crackedDMCD THRESHOLD FWD LWR CORNER SEAL DEPRESSOR ATTACH BRACKET CRACKED AT BS 481, WL 207. *S/D* REMOVED AND REPLACED SEAL DEPRESSOR ATTACH BRACKET PER SRM 51-30-2.SDR 01FDEA00672Bracket · crackedDURING ROUTINE INSP DISCOVERED MCD THRESHOLD AFT LWR CORNER SEAL DEPRESSOR ATTACH BRACKET CRACKED BS 619, WL 207. *S/D* REMOVED AND REPLACED SEAL DEPRESSOR ATTACH BRACKET PER SRM 51-30-2.SDR 01FDEA00715Bracket · crackedN 836 HFEC IND CRACK IN FAILSAFE CHORD AT BS 560, STR 21L, WL 178. R&R CHORD PER SRM 51-20-1 & 51-30-2.SDR 01FDEA00678Stringer · crackedN 1426 STRINGER 16L CRACKED AT BS 623. ** S/D ** COMINGSDR 01FDEA00630Pressure Panel · crackedCRACK INSIDE RIGHT NOSE WHEEL WELL SIDE PANEL BS 268, RBL 23, WL 188. *S/D* REMOVED AND REPLACED SKIN PER SRM 51-30-2.SDR 01FDEA00674Stringer · crackedN 1426 STRINGER 16L CRACKED AT BS 623. ** S/D ** COMINGSDR 01FDEA00665Web · crackedN 833 DUR ROUTINE INSP A CRACK FND IN WEB BETWEEN BS 1176.9 & 1183, LBL 46, WL 208. R&R WEB PER IAW FEDEX SRM 51-40-8.SDR 01FDEA00664Frame · crackedHFEC IND A CRACK IN THE FAIL-SAFE CHORD AT BS 560, STR 21L, WL 178.SDR 01FDEA00633Skin · bulgedN 306 BULGE IN SKIN NEAR LAP JOINT AT BS 298 BETWEEN STR 17L & 18L. ** S/D ** COMINGSDR 01FDEA00625Fitting · corrodedDURING INSP FOUND SUPPORT FITTING FOR NOSE LANDING GEAR DOOR ACTUATOR RODS CORRODED. R&R FITTING PER SRM 51-30-2.SDR CA010813012Door Frame · cracked(CAN) FWD FRAME OF AFT CARGO DOOR CRACKED AT BS1057, STR.24. CRACK MEASURED 1.5 INCHES.SDR 01FDEA00583Actuator · inoperative01-243 AFT DEPART WHEN FLAPS WERE RETRACTED TO 2 DEG #5 SLAT W/N RETRACT. R&R ACTUATOR PER 27-81-032-4. LEAK OPS CK GOOD.SDR 01FDEA00562Engine · faultyENGINE FIRE NR 3 AFT T/O AT 100 FT. FIRED BOTH BOTTLES. *S/D* REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0501-03. OK FOR SERVICE.SDR CA010809014Nut · split(CAN) UPON SCHEDULED MLG REMOVAL FOUND NUT P/N NAS679A5 ON RT SUPPORT ASSY TRUNNION SPLIT ON ONE SIDE.SDR 01FDEA00501Battery · dischargedDURING ROUTINE INSP FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT FOUND INOPERATIVE. *S/D* REMOVED AND REPLACED BATTERY PER IAW BAC 727 MM 33-50-121-2.SDR 01FDEA00500Skin · crackedN 318 DUR ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT BS 303.9 AT STR 4L LWR FASTENER HOLE. R&R FASTENER PER IAW BAC 727 SRM 51-30-2.SDR 01FDEA00499Bracket · crackedN 500 DUR ROUTINE INSP IB BRACKET ON THE #8 FLAP TRACK FOUND CRACKED. R&R & FAB BRACKET PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00498Skin · crackedN 501 DUR ROUTINE INSP RH OB AILERON IB LE SKIN FOUND CRACKED. ** S/D ** R&R BRACKET PER IAW BAC 727 SRM 51-30-2.SDR DHL2001707008Brake · malfunctionedAT 38 DEGREES C IN SMF, ANTI-SKID REPEATEDLY RELEASED AS T/O THRUST WAS SET WITH BRAKES ON. FORWARD MOVEMENT OF ACFT WAS MINIMAL. DID NOT OBSERVE RELEASE LIGHTS (DID NOT LOOK). ANTI-SKID NORMAL ON LANDING. ANTI-SKID SYS IS DEFERRED PER MEL32-5, ASSIGNED DMISDR DHL2001707007Autopilot Sys · malfunctionedWHEN OPERATING AUTOPILOT IN MANUAL MODE USING TURN MODE AUTOPILOT WILL NOT TURN RIGHT. ALL OTHER FUNCTIONS NORMAL. DEFFERED TO DMI 5936, PER MEL 22-1 CAT B, ITEM PLACARD. OPS CHECKED IAW MM 22-11-01, SYSTEM GROUND CHECKS GOOD. PER CREW COMMENT & B727 AUTO-SDR 01FDEA00399Shutoff Valve · failedDURING CLIMB LWR AFT BODY OVERHEAT LIGHT ILLUM. NR 3 BLEED ON, RT PACK ON TURN RT PACK OFF, LIGHT EXTINGUISHED. Removed and replaced RT PURGE LINE SHUTOFF VALVE PER MM 36-13-011-4. LEAK CK OK.SDR 01FDEA00394Unknown · odorUNIDENTIFIED ODOR NOTICED IN FLT. FOLLOWED APPROPRIATE QUICK REF HANDBOOK CK LIST. INSP AIRCRAFT NO CONTAMINATION FOUND.SDR DHL2001707006Computer · malfunctionedWITH AUTOPILOT IN AUTO G/S MODE, AND GLIDE SLOPE CAPTURED, THE AIRCRAFT PITCHES UP AND DOWN AND MAY OR MAY NOT RECOVER TO GLIDE PATH. REPLACED PITCH CHANNEL COMPUTER WITH A SERVICABLE UNIT IAW B727 M/M 22-11-121. CHECKS GOOD AT THIS TIME IAW B727 M/M 22-11-0SDR 01FDEA00345Skin · corrodedDURING ROUTINE INSP FUSELAGE SKIN FOUND BULGING and CORRODED FROM BS 1154 - 1180 AT STR 19L. *S/D* Removed and replaced PER IAW FEDEX EA 7-5710-57242.SDR 01FDEA00344Web · corrodedDURING ROUTINE INSP CTR WING BOX FOUND CORRODED AT BS 870 NEXT TO LWR SPAR CHORD. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5710-57245.SDR 01FDEA00346Skin · corrodedDURING ROUTINE INSP FUSELAGE SKIN FROM BS 1166 - 1173 BETWEEN STR 20L & STR 21L FOUND BULGING AND CORRODED. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5710-57242.SDR 01FDEA00343Angle · corrodedDURING ROUTINE INSP CTR WING BOX AFT SPAR LWR CHORD ANGLE FOUND CORRODED. R&R PER 727 SRM 57-10-1 FIG 3, 51-10-2.SDR 01FDEA00334Skin · crackedDURING ROUTINE INSP FUSELAGE SKIN Found CRACKED AT BS 250.5 BELOW LT NR 3 COCKPIT. *S/D* Removed and replaced DAMAGE PER IAW FEDEX EA 7-5330-57544.SDR 01FDEA00330Intercostal · crackedDURING ROUTINE INSP INTERCOSTAL EXTENTION FROM BS 440-460, STR 2L FOUND CRACKED AT 3RD FASTENER FROM AFT END UPPER ROW 12 O''CLOCK. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-30-2.SDR 01FDEA00332Rib · crackedDURING ROUTINE INSP NR 2 SLAT RIB AT SLAT BS 342 FOUND CRACKED. *S/D* REMOVED AND REPLACED NR 2 L/E SLAT PER IAW BAC 727 MM 27-81-011.SDR 01FDEA00333Rib · crackedDURING ROUTINE INSP NR2 SLAT RIB AT SLAT BS 347 FOUND CRACKED. *S/D* REMOVED AND REPLACED PER IAW BAC 727 MM 27-81-011.SDR 01FDEA00336Seat Track · crackedDURING ROUTINE INSP NR 2 MAIN CABIN SEAT TRACK FOUND CRACKED AT BS 870.SDR 01FDEA00323Pump · failedON T/O NR 1 ENG SHUTDOWN. ENG MET ALL RESTART PREM. REMOVED AND REPLACED NR 1 ENG FUEL CONTROL UNIT AND FUEL PUMP PER JRH, LEAK CK GOOD. OK FOR SERVICE.SDR 01FDEA00284Fire Warning · false activationFIRE WARNING BELL CAME ON IMMED AFT T/O. ENG FIRE AND WHEEL WELL FIRE SYS TEST NORMAL. APU FIRE SYS DID NOT. INSP APU FIRE SYS AND APU. FOUND SYS TO TEST NORM AND NO PROBLEMS IN THE APU AREA. TEST APU SEVERAL TIMES AND SYS CK GOOD. OK FOR SERVICE. ALL ESDR DHL2001707005Light · damagedRIGHT TAIL NAV LIGHT ASSY DAMAGED BY BAGGAGE CART. REPLACED RT WING TIP ASSY IAW MM 57-20-0. STATUS: CLOSED.
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