# Service difficulty reports: N536DA, cancelled Jul 20, 2010 A list on [N536DA, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N536DA-2010-07-20.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL72S010865](https://openairdocs.org/sdr/DL72S010865.md): Sign · inoperative · May 29, 2001 · N536DA · Boeing 727232 · Emergency Lighting > EMERGENCY EXIT SIGN INOP ACROSS FROM ROW 32. RELAMPED EMERGENCY EXIT SIGN. - [SDR DL72S010260](https://openairdocs.org/sdr/DL72S010260.md): Engine · intermittent · Feb 14, 2001 · N536DA · Boeing 727232 · Engine (Turbine/Turboprop) > NR 1 ENG FILTER BY PASS LIGHT ILLUMINATED ON TAKEOFF ROLL AT 100 KTS. RETURNED TO BLOCKS. INSP AND REPLACED NR 1 ENG MAIN OIL SCREEN. FWD FILTER BY PASS LIGHT TO MCO AND PLACARD PER MEL 79-00-02. - [SDR DL72S001547](https://openairdocs.org/sdr/DL72S001547.md): Spar · cracked · Aug 11, 2000 · N536DA · Boeing 727232 · Elevator Structure > THE RT ELEVATOR WAS FOUND WITH A.25 INCH CRACK IN THE REAR SPAR EMANATING FROM THE EDGE OF A SHEAR PLATE. THE CRACK IS TYPICAL OF BAC S/B 727-55-0089. HOWEVER, THE TERMINATING ACTION OF THE S/B HAD BEEN ACCOMPLISHED. THE CRACK WAS STOP DRILLED AND ALLOWED - [SDR DL72S001383](https://openairdocs.org/sdr/DL72S001383.md): Light · inoperative · Jul 21, 2000 · N536DA · Boeing 727232 · Emergency Lighting > OVERHEAD EMERGENCY LIGHT INOP AT STA 680. REPLACED LIGHT ASSY, OPS NORMAL. - [SDR DL72S000966](https://openairdocs.org/sdr/DL72S000966.md): Skin · cracked · May 15, 2000 · N536DA · Boeing 727232 · Fuselage Main, Plate/Skin > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC CONFIRMED CRACKS IN TWO FRAME BAYS. BECAUSE OF THE CRACKS AND EXISTING PREVIOUS REPAIRS THE ENTIRE LAP JOINT - [SDR DL72S000842](https://openairdocs.org/sdr/DL72S000842.md): Power Supply · inoperative · Apr 28, 2000 · N536DA · Boeing 727232 · Emergency Lighting > DURING CHECK OF THE EMERGENCY LIGHT SYSTEM, ROWS AFT OF 26 AND THE LT, RT AND AFT DOOR WERE INOP. FOUND AFT POWER SUPPLY BAD. REPLACED THE POWER SUPPLY, OPS CHECK GOOD. - [SDR DL72S000644](https://openairdocs.org/sdr/DL72S000644.md): Panel · missing · Apr 5, 2000 · N536DA · Boeing 727232 · Engine Cowling System > FWD BLOW OUT PANEL ON RT SIDE OF NR 2 ENG COWL MISSING. REPLACED BLOW OUT PANEL, NO DUCT LEAKS NOTED ON ENG RUN. - [SDR DL72S000187](https://openairdocs.org/sdr/DL72S000187.md): Skin · cracked · Jan 25, 2000 · N536DA · Boeing 727232 · Fuselage Main, Plate/Skin > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK IN THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION CONFIRMED THREE CRACKS BETWEEN FS 520 & FS 540. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EX - [SDR DL72S991416](https://openairdocs.org/sdr/DL72S991416.md): Track · corrosion · Jun 23, 1999 · N536DA · Boeing 727232 · Trailing Edge Flaps > CORROSION WAS DISCOVERED IN THE TWO BOLT HOLES WHERE THE I/B FLAP O/B FLAP TRACK ATTACHES TO THE SPOILER SUPPORT LWR CHORD. REWORKED PER ERA 333256-14, REV A. - [SDR DL72S991415](https://openairdocs.org/sdr/DL72S991415.md): Fitting · corroded · Jun 23, 1999 · N536DA · Boeing 727232 · Vertical Stabilizer > RHS BOLT HOLES FOR THE VERT FIN FITTING ATTACH TO TENSION TIE RIB WAS FOUND WITH CORROSION. REWORKED PER ERA 333260-14, REV B. - [SDR DL72S991407](https://openairdocs.org/sdr/DL72S991407.md): Frame · cracked · Jun 21, 1999 · N536DA · Boeing 727232 · Fuselage Main, Frame > DURING ACCOMPLISHMENT OF INSPECTIONS OF THE OVERWING EXIT FRAMES, UNIDENTIFIED REPAIRS WERE NOTED. THE SUBJECT ERA WILL EVALUATE THE REPAIRS AND ENSURE COMPLIANCE / DOCUMENTATION. REWORKED PER ERA 333213-14AD, REV A. - [SDR DL72S991360](https://openairdocs.org/sdr/DL72S991360.md): Frame · cracked · Jun 16, 1999 · N536DA · Boeing 727232 · Fuselage Main, Frame > FRAME AT BS 620 WAS FOUND CRACKED REMOVAL OF THE CRACK REQUIRED REMOVAL OF APPROX 5 OF THE UPPER FLANGE FROM THE PRODUCTION SPLICE AT RBL 11 INBD TO RBL 6. REPAIRED PER ERA 333235-14. - [SDR DL72S991359](https://openairdocs.org/sdr/DL72S991359.md): Skin · gouged · Jun 16, 1999 · N536DA · Boeing 727232 · Fuselage Main, Plate/Skin > GOUGE FOUND IN FUSELAGE SKIN AT AFT EDGE OF THE C2 DOOR AT BS 990. DAMAGE AREA IS LOCATED AT S24R PLUS 5 AND IN THE SKIN ONLY. REPAIRED PER ERA 333244-14, REV A. - [SDR DL72S990745](https://openairdocs.org/sdr/DL72S990745.md): Skin · cracked · Apr 3, 1999 · N536DA · Boeing 727232 · Fuselage Main, Plate/Skin > LFEC INSPECTION OF THE STINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENG - [SDR DL72S990408](https://openairdocs.org/sdr/DL72S990408.md): Light · inop · Feb 26, 1999 · N536DA · Boeing 727232 · Emergency Lighting > L1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS NOW OK. - [SDR DL72S982252](https://openairdocs.org/sdr/DL72S982252.md): Coffeemaker · failed · Oct 31, 1998 · N536DA · Boeing 727232 · Buffet/Galleys > INDICATION OF SMOKE OBSERVED BY FLT ATTEND IN AFT GALLEY AND AFT CABIN. REPLACED COFFEEMAKER AND CANNON PLUG. - [SDR DL72S982241](https://openairdocs.org/sdr/DL72S982241.md): Connector · shorted · Oct 31, 1998 · N536DA · Boeing 727232 · Buffet/Galleys > SMOKE IN AFT CABIN. FOUND THE CANNON PLUG FOR THE NR 3 COFFEEMAKER IN THE AFT GALLY SHORTED. PULLED AND COLLARD C/B, DISCONNECTED CANNON PLUG FROM COFFEEMAKER. - [SDR DL72S981541](https://openairdocs.org/sdr/DL72S981541.md): Wire · broken · Jul 20, 1998 · N536DA · Boeing 727232 · Light System Wiring > THE FWD EMER EXIT SIGN IN THE COACH CABIN INOP. FOUND BROKEN GRD WIRE AT C/P FOR LIGHT ON LIGHT SIDE. REPAIRED WIRE, EMER LIGHTS CK OK. - [SDR DL72S980690](https://openairdocs.org/sdr/DL72S980690.md): Bracket · cracked · Mar 30, 1998 · N536DA · Boeing 727232 · Leading Edge Slat Actuator > FOUND ON D1 LETTER CK, NR 2 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER RADIUS. REPAIRED PER MM 57-20-21. - [SDR DL72S980689](https://openairdocs.org/sdr/DL72S980689.md): Web · cracked · Mar 30, 1998 · N536DA · Boeing 727232 · Fuselage Miscellaneous Structure > FOUND ON D1 LETTER CK, LT VERT TORQUE BOX WEB CRACKED AT UPPER END AT STA 1237 LT. REPAIRED PER MM 53-11-0. - [SDR DL72S980673](https://openairdocs.org/sdr/DL72S980673.md): Indicator · shorted · Mar 27, 1998 · N536DA · Boeing 727232 · Flight Compartment Lighting > AT FL 310 HAD STRONG ELECT SMELL LIKE PLASTIC BURNING. INDICATOR LTS MASTER SECT 1 C/B POPPED. ODOR SLOWLY SUBSIDED, FOUND COCKPIT INDICATOR SHORTING TO GROUND. REPOSITIONED TERMINALS, CKS OK. - [SDR DL72S972645](https://openairdocs.org/sdr/DL72S972645.md): Structure · damaged · Dec 10, 1997 · N536DA · Boeing 727232 · Fuselage Main, Structure > FUSELAGE, SKIN, FRAME, AND STRINGER FS228-252, S24R. REPAIR FOR DENTED AND CRACKED SKIN, STRINGERS, AND FRAMES. THE FUSELAGE SKIN BETWEEN FS 228 AND 252 AT S-24R WAS DAMAGED BY GROUND EQUIPMENT. THE SKIN DAMAGE WAS CUTOUT AND A DOUBLER REPAIR INSTALLED. TH - [SDR DL72S971692](https://openairdocs.org/sdr/DL72S971692.md): Stringer · cracked · Aug 28, 1997 · N536DA · Boeing 727232 · Vertical Stabilizer > 1.25 INCH CRACK IN VERT STAB S-9R AND SECOND BULKHEAD ABOVE CRAWL WAY OPENING. REPAIRED PER MM 55-30-0 PG 803. - [SDR DL72S970112](https://openairdocs.org/sdr/DL72S970112.md): Frame · cracked · Jan 20, 1997 · N536DA · Boeing 727232 · Fuselage Main, Frame > A.375 INCH VISIBLE CRACK IN MLG UPLOCK FRAME OUTB'D FLANGE STA 913.5 UPPER END OF RADIUS BLOCK. INSTALLED REPAIR PER MM 53-11-0 PG 834. - [SDR DL72S970110](https://openairdocs.org/sdr/DL72S970110.md): Skin · cracked · Jan 20, 1997 · N536DA · Boeing 727232 · Elevator, Plate/Skin > FOUND DURING C-1 LETTER CHECK, 4.5 INCH CRACK LEFT ELEVATOR LWR SKIN AT O/B END. REPAIRED PER SRM 55-20-3. - [SDR DL72S961515](https://openairdocs.org/sdr/DL72S961515.md): Web · cracked · Jun 24, 1996 · N536DA · Boeing 727232 · Fuselage Miscellaneous Structure > A 1.25 IN CRACK IN TORQUE BOX WEB UPPER RT CORNER AT STA 1213 AT UPPER CORD. INSTALLED DOUBLER PER MM 53-11-0 PG 832. - [SDR DL72S960174](https://openairdocs.org/sdr/DL72S960174.md): Spar · cracked · Jan 24, 1996 · N536DA · Boeing 727232 · Leading Edge Devices > DURING SHOP INSPECTION FOR WING SLAT PANEL, FOUND LEADING EDGE SPAR HAD A TEMPORARY REPAIR. REPAIRED SPAR PER MM 7-54-0 FIG 802 A. - [SDR DL72S960173](https://openairdocs.org/sdr/DL72S960173.md): Ballast · failed · Jan 23, 1996 · N536DA · Boeing 727232 · Passenger Compartment Lighting > CEILING POWER FWD C/B ON P18-3 PNL POPPED FOLLOWED BY AN ACRID ELECTRICAL SMELL IN THE FWD PART OF THE AIRCRAFT. PULLED AND COLLARED FWD CONT C/B AND FWD CEILING PWR C/B. PULLED C/P ON CEILING LIGHT AT RT ROW 24 AND LT 17. FOUND BURNED BALLAST, REPLACED BAL - [SDR DL72S954668](https://openairdocs.org/sdr/DL72S954668.md): Mask · popped indicator · Dec 7, 1995 · N536DA · Boeing 727232 · Portable Oxygen System > DURING INSPECTION, FOUND FWD CABIN PBE WITH POPPED INDICATOR. REPLACED PBE. - [SDR DL72S954476](https://openairdocs.org/sdr/DL72S954476.md): Angle · cracked · Nov 22, 1995 · N536DA · Boeing 727232 · Leading Edge Devices > FOUND DURING B-1 LETTER CHECK, NR 5 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED.25 INCH AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A. - [SDR DL72S954475](https://openairdocs.org/sdr/DL72S954475.md): Actuator Mount · cracked · Nov 22, 1995 · N536DA · Boeing 727232 · Leading Edge Slat Control System > FOUND DURING B-1 LETTER CHECK, NR 7 L/E SLAT ACTUATOR MOUNT FITTING CRACKED 1 INCH AT LWR I/B MOUNT BOLT. REPAIRED PER M/M 57-42-0 PAR 5. - [SDR DL72S954473](https://openairdocs.org/sdr/DL72S954473.md): Spar Stiffener · cracked · Nov 22, 1995 · N536DA · Boeing 727232 · Wing Miscellaneous Structure > FOUND ON B1 LETTER CK, LE SPAR STIFFENER CRACKED OUTBD TRACK NUMBER 3 SLAT INBD ANGLE. REPAIRED PER MM 57-20-21. - [SDR DL72S954343](https://openairdocs.org/sdr/DL72S954343.md): Bolt · missing · Nov 11, 1995 · N536DA · Boeing 727232 · Leading Edge Slat Control System > ON DEPARTURE, NR 2 SLAT FAILED TO RETRACT, AIL WAS DISPLACED 30 UNITS, NR 2 SLAT SHOWED GREEN ON S/O PANEL, NR 2 SLAT FINALLY STOWED WITH SPEED REDUCTION. FOUND NR 2 SLAT LWR INBRD BOLT MISSING FROM TRUNNION BRACKET, INTERMITTENTLY BINDING SLAT RETRACTION REP - [SDR DL72S953920](https://openairdocs.org/sdr/DL72S953920.md): Angle · cracked · Sep 25, 1995 · N536DA · Boeing 727232 · Wing Miscellaneous Structure > THE NR 5 L/E SLAT, LOWER T/E ATTACH ANGLE CRACKED AT RIB NR 9. REPAIRED PER M/M 57-54-0 PAGE 807A. - [SDR DL72S953394](https://openairdocs.org/sdr/DL72S953394.md): Eel Battery Pack · discharged · Aug 14, 1995 · N536DA · Boeing 727232 · Emergency Lighting > DURING LAYOVER, FOUND EMERGENCY LIGHTS ABOVE AFT AIRSTAIR INOP. REPLACED BATTERY OPERATION NORMAL. - [SDR DL72S952133](https://openairdocs.org/sdr/DL72S952133.md): Angle · cracked · May 15, 1995 · N536DA · Boeing 727232 · Leading Edge Devices > DOUBLER CRACKED FOR FLANGE UNDER ANTI ICE DUCT FOR NR 2 SLAT. FOUND DURING A-2 LTR CK. REPAIRED PER MM 57-54-0. - [SDR DL72S952132](https://openairdocs.org/sdr/DL72S952132.md): Rib · cracked · May 15, 1995 · N536DA · Boeing 727232 · Leading Edge Devices > ONE-HALF INCH CRACK NR 2 SLAT NOSE RIB ANGLE O/B OF ACTUATOR ATTACH. REPAIRED PER MM 57-54-0. FOUND AT A-2 LETTER CHECK. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 n_number = 'N536DA' AND deregistration_id = 'N536DA-2010-07-20' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N536DA-2010-07-20/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.