# Service difficulty reports: Boeing 727-22C

A list on [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 47 · 2,328 reports

- [SDR VGCA2011101400001](https://openairdocs.org/sdr/VGCA2011101400001.md): Mount · cracked · Oct 14, 2011 · N231FL · Boeing 72722C · Engine Mount Section
  > DURING INSPECTION, A CRACK WAS DISCOVERED IN THE NR 3 AFT ENGINE MOUNT.
- [SDR 2011F00025](https://openairdocs.org/sdr/2011F00025.md): Engine · flamed out · Feb 3, 2011 · N231FL · Boeing 72722C · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FLAMEOUT JUST AFTER FUEL HEAT SELECTION PRIOR TO DESCENT. ENGINE RESTART IAW NORMAL PROCEDURES ACCOMPLISHED. ALL PARAMETER NORMAL AFTER INFLIGHT RESTART. PROCEEDED TO NORMAL LANDING AT AIRPORT.
- [SDR CA080425002](https://openairdocs.org/sdr/CA080425002.md): Warning Switch · closed · Apr 21, 2008 · Boeing 72722C · Stabilizer Control System
  > (CAN) WHILE ATTEMPTING TAKEOFF, TAKEOFF WARNING INTERMITTENT, HORN SOUNDED UPON POWER LEVER ADVANCEMENT. TAKEOFF WAS ABORTED AND AC RETURNED TO BLOCKS. TROUBLESHOOTING REVEALED THE LOWER HORIZONTAL STABILIZER TAKEOFF WARNING SWITCH WAS NOT CONTACTING ACTUATING
- [SDR CA080401002](https://openairdocs.org/sdr/CA080401002.md): Blade · damaged · Mar 13, 2008 · Boeing 72722C · Turbine Engine Compressor Section
  > (CAN) WHILE PERFORMING AC DAILY INSP, NR (3) ENGINE C-1 FAN ASSY WAS FOUND TO HAVE SUBSTANTIAL DAMAGE TO (3) BLADES. THE (3) BLADES HAD SIGNIFICANT L/E DEFORMATION WITH ONE EXHIBITING VISUAL CRACKING. THE C-1 FAN WAS REMOVED FROM SERVICE AND REPLACED. THE AC
- [SDR UPS07250122](https://openairdocs.org/sdr/UPS07250122.md): Slide · out of position · Jul 5, 2007 · N944UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE:N/A EMERGENCY SLIDE TORN OFF CABIN/COCK PIT ENTRY DOOR, UNABLE TO REINSTALL. DEF YBDER N353884. INSTALLED EVAC SLIDE MAIN CABIN DOOR PER MM CHAP 25-60-14-2.
- [SDR UPS07250083](https://openairdocs.org/sdr/UPS07250083.md): Slide · inoperative · Jun 27, 2007 · N944UP · Boeing 72722C · Escape Slide
  > CREW SLIDE FELL OUT OF CONTAINER WHEN THE ENTRY DOOR WAS OPENED. REINSTALLED EVACUATION SLIDE IN THE CONTAINER IAW MM 52-25-60-14-2.
- [SDR UPS07250056](https://openairdocs.org/sdr/UPS07250056.md): Slide · inoperative · Jun 26, 2007 · N944UP · Boeing 72722C · Escape Slide
  > ESCAPE SLIDE IS OUT OF PACK. REINSTALLED EVACUATION SLIDE IAW AMM 25-60-14-2.
- [SDR UPS07249849](https://openairdocs.org/sdr/UPS07249849.md): Battery Pack · inoperative · May 23, 2007 · N942UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CABIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHT IAW B727 MM 33-50-67-2. OPS CHECKS NORMAL.
- [SDR UPS07249643](https://openairdocs.org/sdr/UPS07249643.md): Guide Arm · out of adjust · Apr 20, 2007 · N945UP · Boeing 72722C · Flight Compartment Windows
  > INSPECTION TYPE:N/A CAPTAIN'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED GUIDE PIN OF CAPTAIN'S SLIDING WINDOW WITH REF TO MM 56-12-11-5. WINDOW OPERATES AND SECURES LOCKED NORMAL.
- [SDR UPS06248764](https://openairdocs.org/sdr/UPS06248764.md): Slide · dislodged · Dec 12, 2006 · N945UP · Boeing 72722C · Escape Slide
  > ESCAPE SLIDE FELL OUT OF HOUSING. REINSTALLED ESCAPE SLIDE.
- [SDR UPS06248725](https://openairdocs.org/sdr/UPS06248725.md): Slide · out of position · Nov 30, 2006 · N944UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE: N/A MAIN ENTRY DOOR ESCAPE SLIDE FALLS OUT OF ITS CONTAINER WHEN DOOR IS MOVED. FOUND COMPARTMENTAL COVER LATCH CABLE DISCONNECTED. REPAIRED IAW 25-60-14-2. OPS CK GOOD.
- [SDR UPS06248609](https://openairdocs.org/sdr/UPS06248609.md): Battery · discharged · Nov 12, 2006 · N930UP · Boeing 72722C · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM 35-50-67. OPS CHECK GOOD.
- [SDR UPS06248335](https://openairdocs.org/sdr/UPS06248335.md): Slide · dislodged · Oct 5, 2006 · N944UP · Boeing 72722C · Escape Slide
  > ESCAPE SLIDE FELL OUT OF STORAGE HOUSING IN FLIGHT. ATTEMPTED TO RESTORE SLIDE. REPACKED SLIDE ASSY AS REQUIRED.
- [SDR UPS06248018](https://openairdocs.org/sdr/UPS06248018.md): Actuator · worn · Sep 21, 2006 · N942UP · Boeing 72722C · Leading Edge Slat Actuator
  > LED NR 6 DOES NOT RETRACT. THE AMBER LT CAME ON DURING CLIMB TO 310. COULD NOT DUPLICATE FAULT ON GROUND. AS PRECAUTION REPLACED NR 6 L/E SLAT ACTUATOR. OPS CHECK GOOD, REF MM 27-81-32-4.
- [SDR UPS06248005](https://openairdocs.org/sdr/UPS06248005.md): Actuator · illuminated · Sep 19, 2006 · N945UP · Boeing 72722C · Landing Gear Position and Warning
  > ALL 3 RED GEAR UNSAFE LIGHTS ILLUMINATED ACCOMPANIED BY TAIL SKID DOWN INDICATION. FERRY PERMIT 9007. REMOVED & REPLACED TAIL SKID ACTUATOR. OPS CHECK GOOD AT THIS DATE PER MM 32-71-12-4. PERFORMED MAIN GEAR & NOSE GEAR RETRACTION EXTENSION PER MM 32-32-005,
- [SDR 2007FA0000197](https://openairdocs.org/sdr/2007FA0000197.md): Ring · elongated · Sep 4, 2006 · N942UP · Boeing 72722C · Escape Slide
  > DURING ROUTINE C-CHECK INSPECTION OF FORWARD DOOR EMERGENCY ESCAPE SLIDE, THE SLIDE BUSTLE LATCH CHAIN WAS FOUND DETACHED FROM THE SPLIT RING. THE SPLIT RING HAD BECOME ELONGATED AND THE RING COILS HAD SEPARATED THUS ALLOWING THE CHAIN TO DETACH. THE SLIDE W
- [SDR NACA20060049](https://openairdocs.org/sdr/NACA20060049.md): Line · loose · Sep 1, 2006 · N792A · Boeing 72722C · Turbine Engine Oil System
  > NR 1 ENGINE OIL QUANTITY DECREASED TO ZERO. ENGINE SHUTDOWN. FOUND GEARBOX OIL PRESSURE LINE LOOSE. ENGINE REPLACED FOR UNABLE TO CONFIRM POSITIVE OIL PRESSURE DURING WINDMILLING AFTER SHUTDOWN.
- [SDR UPS06247858](https://openairdocs.org/sdr/UPS06247858.md): Hinge · cracked · Aug 24, 2006 · N942UP · Boeing 72722C · Ailerons
  > INSPECTION TYPE:C CRACK FOUND AFT FASTENER HOLE OF LT O/B AILERON 2ND FROM I/B FIXED W WING HINGE CASTING UPPER O/B FLANGE. REPLACE HINGE ASSY. HINGE ASSY REPLACED IAW SRM 51-30-2, 51-30-5 AND MM 27-10-14, 21-80-01 AND BOEING DRAWING 65-19275. REF NRC 10080
- [SDR UPS06247770](https://openairdocs.org/sdr/UPS06247770.md): Panel · delaminated · Aug 20, 2006 · N941UP · Boeing 72722C · Wing, Plate/Skin
  > LEFT WING OUTBOARD PANEL DELAMINATED. REMOVED DAMAGED AREA OF SKIN PER SRM 51 40 24. MADE REPAIR PARTS TREATED WITH AC 130 SOLGEL. REF SRM 51 40 20, PG 42 46. APPLIED PRIMER BARED AFT 175* PER SRM 51 40 24 FIG 2.
- [SDR UPS06247849](https://openairdocs.org/sdr/UPS06247849.md): Fairing · corroded · Aug 18, 2006 · N942UP · Boeing 72722C · Aerodynamic Fairings
  > INSPECTION TYPE:C BODY FAIRING 3430 HAS AREA OF LIGHT SURFACE CORROSION LWR DOOR CUTOUT FRAME. PLEASE REMOVE ANCHOR NUTS, REMOVE CORROSION, REINSPECT AND RECTIFY AS NECESSARY. FRAME AND SUPPORT BRACKET REPAIRED IAW SRM 51-40-04 AND 51-30-02.
- [SDR UPS06247815](https://openairdocs.org/sdr/UPS06247815.md): Bushing · corroded · Aug 15, 2006 · N942UP · Boeing 72722C · Engine Mount Section
  > INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON REPAIR BUSHING IN AFT OB HOLE FITTING REPAIR BUSHING REMOVED IAW SOPM 20-50-03. REPAIR CARRIED OUT IAW APPX B.
- [SDR UPS06247804](https://openairdocs.org/sdr/UPS06247804.md): Bracket · cracked · Aug 15, 2006 · N942UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF LT 870 FITTING AT LWR CORNER, CRACK IDENTIFIED ON BRACKET REMOVED BRACKET IAW SRM 51-30-02. NEW BRACKET INSTALLED IAW SRM 51-30-02 AND DRAWING NR 65-25370.
- [SDR UPS06247806](https://openairdocs.org/sdr/UPS06247806.md): Skin · scratched · Aug 14, 2006 · N942UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SCRATCH ON FUSELAGE SKIN BETWEEN BS 1186 AND 1193 S19R. PAINTSTRIP AREA A RE-INSPECT AND RECTIFY AREA PAINT STRIPPED IAW MM 51-20-01. SCRATCH OUTSIDE LIMITS IAW SRM 5 3-30-1. REPAIR CARRIED OUT IAW SRM 53-30-03 AND 51-30-02.
- [SDR UPS06247897](https://openairdocs.org/sdr/UPS06247897.md): Ring · broken · Aug 11, 2006 · N942UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE-C ON SLIDE LATCH CHAIN AND RING BROKEN ON FWD ENTRY DOOR ESCAPE SLIDE. REPLACE RING AND CHAIN ON FURTHER INVESTIGATION CHAIN FOUND NOT TO BE BROKEN, BUT RING WAS DEFORMED AND DETACHED. RING REPLACED IAW MM 25-60-14. NOTE: RING SOLDERED W/NO D
- [SDR UPS06247831](https://openairdocs.org/sdr/UPS06247831.md): Skin · cracked · Aug 11, 2006 · N942UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE-C CRACK ON RT OB FORE FLAP LE AT CUTOUT OB OF IB SEQUENCE CARRIAGE ATTACH BRACKET DAMAGE OUTSIDE LIMITS IAW SRM 57-50-1. CRACK STOP DRILLED IAW SRM 57-5 0-4. HFEC CARRIED OUT IAW NDTM 51-00-00 PT 6 FIG 4 CRACK CONTAINE D. REPAIR CARRIED OUT I
- [SDR UPS06247830](https://openairdocs.org/sdr/UPS06247830.md): Support · cracked · Aug 10, 2006 · N942UP · Boeing 72722C · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE-C ENGINE NR 2 SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL HAS SUSPECT CRACK ON RT CHORD BETWEEN AFT CONE BOLT HOUSING AND REAR SPAR AT 2 FOOT FROM TOP OF CHORD HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. CRACK CONFIRMED. CHORD REPLACED IAW DR
- [SDR UPS06247823](https://openairdocs.org/sdr/UPS06247823.md): Floorbeam · corroded · Aug 9, 2006 · N942UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-C CORROSION AT BS 344 OUTSIDE LIMITS, PLEASE REPAIR IAW SRM FLOORBEAM TOP CHORD REMOVED IAW SRM 51-30-02. SPLICE ANGLES AND TOP CHORD FABRICATED IAW SRM 53-10-08. PARTS REPROTECTED IAW SRM 51-10-02. PARTS INSTALLED IAW SRM 51-30-02.
- [SDR UPS06247745](https://openairdocs.org/sdr/UPS06247745.md): Floorbeam · corroded · Aug 9, 2006 · N942UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C, ON REMOVAL OF FLOOR PANEL AT ENTRANCE TO COCKPIT. CORROSION FOUND ON FLOORBEAM TOP CAP BS 344 LBL 10 TO RBL 12. AREA FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1.
- [SDR UPS06247721](https://openairdocs.org/sdr/UPS06247721.md): Pressure Panel · cracked · Aug 8, 2006 · N942UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C SUSPECT CRACK ON NLG SIDE WALL AT WL 184 BS 276. CRACK REPAIRED IAW SRM 51-40-02.
- [SDR UPS06247469](https://openairdocs.org/sdr/UPS06247469.md): Light · inoperative · Jul 27, 2006 · N941UP · Boeing 72722C · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT INOP IN ON POSITION. REMOVED AND REPLACED EMERGENCY LIGHT ASSY.
- [SDR UPS06247467](https://openairdocs.org/sdr/UPS06247467.md): Light · inoperative · Jul 27, 2006 · N941UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHT INOP IN ON POSITION. REMOVED AND REPLACED C/P EMERGENCY LIGHT ASSY IAW MM 33-50-67-2. SYSTEM OPS OK.
- [SDR UPS06247746](https://openairdocs.org/sdr/UPS06247746.md): Pressure Panel · cracked · Jul 26, 2006 · N942UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, DURING PRESSURIZATION CHECK LEAK WAS FOUND IN NOSE WW PRESSURE DECK CE CEILING. WEB CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-02, 51-10-02 & 51-10-01.
- [SDR NACA20060041](https://openairdocs.org/sdr/NACA20060041.md): Skin · cracked · Jul 22, 2006 · N792A · Boeing 72722C · Fuselage Main, Plate/Skin
  > CORRODED CRACK ON RT FUSELAGE AT STA. 1085-1088 BETWEEN S-12 AND S-13.INSTALLED FUSELAGE SKIN REPAIR BETWEEN BS 1080-1100 AND STRINGERS 12R-14R. REPAIR SKETCH 1-211756245. DOA-300064-NM FORM 8100-9 DATED 22 JULY 2006.
- [SDR NACA20060040](https://openairdocs.org/sdr/NACA20060040.md): Pin · installed · Jun 17, 2006 · N727YK · Boeing 72722C · Landing Gear Retraction/Extension System
  > NOSE GEAR WOULD NOT RETRACT AT GEAR UP. REMOVED NOSE GEAR PIN FROM NOSE GEAR.
- [SDR UPS06247060](https://openairdocs.org/sdr/UPS06247060.md): Frame · cracked · Jun 1, 2006 · N944UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE:C DURING REMOVAL OF FASTENERS TO FACILITATE THE FLOOR SUPPORT REPAIR FOR NRC 100734 CRACK FOUND ON FRAME FOR INNER RADIUS BS1050 RBL 12. CRACKED FRAME AT ABOVE LOCATION REPAIRED IAW SRM 53-10-02 AND SRM 51-4 0-3
- [SDR UPS06247095](https://openairdocs.org/sdr/UPS06247095.md): Spar · cracked · May 26, 2006 · N944UP · Boeing 72722C · Elevator, Spar/Rib
  > INSPECTION TYPE:C ON INSP CRACK DETECTED ON THE LEFT ELEVATOR REAR SPAR STA 138 APPROX. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. ELEVATOR REMOVED IAW MM 27-30-01. NEW ELEVATOR INSTALLED IAW MM 27-30-01. ELEVATOR FRI
- [SDR UPS06247080](https://openairdocs.org/sdr/UPS06247080.md): Floor Support · cracked · May 26, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FLOOR SUPPORT FOUND TO BE CRACKED AT BS 1060 LBL 6. DAMAGE CUT OUT IAW SRM 53-10-05. FASTENERS REMOVED IAW SRM 51-30-02. REPAIR PARTS FABRICATED IAW SRM 53-10-05 AND REPROTECTED IAW SRM 51-10- 02. REPAIR PARTS INSTALLED IAW SRM 51-30-02.
- [SDR UPS06247004](https://openairdocs.org/sdr/UPS06247004.md): Skin · cracked · May 26, 2006 · N944UP · Boeing 72722C · Passenger/Crew Doors
  > INSPECTION TYPE:C SUSPECT SKIN CRACK IN AFT AIRSTAIRS SKIN AT THE NR 8 STEP FROM THE BOTTOM POSITION. CARRY OUT NDI AND RECTIFY AS NECESSARY. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONFIRMED, ENDS MARKED. REPAIR CARRIED
- [SDR UPS06247061](https://openairdocs.org/sdr/UPS06247061.md): Floor Support · cracked · May 25, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO BAY CRACK ON FLOOR SUPPORT AT BS 1060 RBL 0. DAMAGED AREA CUT OUT IAW SRM 53-10-05. FASTENERS REMOVED IAW SRM 51-30 -02. REPAIR PARTS FABRICATED IAW SRM 53-10-05. REPAIR PARTS REPROTECTED IAW SRM 51-10-02. REPAIR PARTS INSTALLED IA
- [SDR UPS06247055](https://openairdocs.org/sdr/UPS06247055.md): Web · cracked · May 25, 2006 · N944UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C AFT AIRSTAIRS RT LIGHTENING HOLE CRACKED. AREA MARKED, PLS REPAIR IAW SRM REPAIR CARRIED OUT IAW SRM 51-40-2, 51-10-2 & 51-30-2.
- [SDR UPS06247054](https://openairdocs.org/sdr/UPS06247054.md): Web · cracked · May 25, 2006 · N944UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C CRACK ON THE LEFT WEB IN THE AFT AIRSTAIRS AREA MARKED. REPAIR IAW SRM REPAIR CARRIED OUT IAW SRM 51-40-2, 51-10-2 & 51-30-2.
- [SDR UPS06247045](https://openairdocs.org/sdr/UPS06247045.md): Door Frame · cracked · May 25, 2006 · N944UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C AFT CARGO DOOR SUSPECT CRACK ON FRAME AT UPPER AFT DOOR STOP. AREA CLEANED AND REINSPECTED, CRACK CONFIRMED VISUALLY AT AFT UPPER DOOR STOP CUTOUT. DUE TO EXCESSIVE WORK REQUIRED TO REPAIR, DOOR TO BE REPLACED.
- [SDR UPS06247067](https://openairdocs.org/sdr/UPS06247067.md): Floor Support · corroded · May 24, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO BAY BS 1110 RBL20 FLOOR SUPPORT CORRODED AT ANCHOR NUTS LOCATION. TO GAIN ACCESS FLOOR PANEL AND SCUFF PLATE AT CARGO DOOR CUT OUT REMOVED IAW SRM 51-30-02. DAMAGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10* 0-01. DAMAGED SECTION RE
- [SDR UPS06247005](https://openairdocs.org/sdr/UPS06247005.md): Angle · corroded · May 24, 2006 · N944UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C DURING RECTIFICATION OF NRC 100332 ADJACENT ANGLE OF FWD CARGO BLKD UP PER SECTION BS 680 RBL 30 TO 40 FOUND TO BE CORRODED AT ANCHOR NUT LOCATIONS. ON CLEAN UP CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AFT BLKD ANGLE IAW SRM 51-30-2. R
- [SDR UPS06247079](https://openairdocs.org/sdr/UPS06247079.md): Support Angle · cracked · May 23, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C BS660 LT CRACK ON OB SUPPORT ANGLE FOR RAM AIR INTAKE DUCTING AT FASTENER LOCATION. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-30-02. FABRICATED SUPPORT ANGLE AND HEAT TREATED IAW SRM 51-20-1. INSTALLED SUPPORT ANGLE IAW SRM 5 1-30-02.
- [SDR UPS06247078](https://openairdocs.org/sdr/UPS06247078.md): Support · chafed · May 23, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON REMOVAL OF FLOW VENTURI SENSE LINE CROSS SUPPORT STRUCTURAL MEMBER AT LBL 40 BETWEEN BS 1203 AND 1223 FOUND CHAFFED. CROSS STRUCTURAL MEMBER REMOVED IAW SRM 51-30-02. REPLACEMENT REQUIRED. INSTALLED NEW CROSS STRUCTURAL MEMBER IAW SRM 51
- [SDR UPS06247059](https://openairdocs.org/sdr/UPS06247059.md): Spar · cracked · May 23, 2006 · N944UP · Boeing 72722C · Elevator, Spar/Rib
  > INSPECTION TYPE:C X-RAY INSPECTION HAS DETECTED 2 SUSPECT CRACKS ON INSPAR RIBS LOCATED BETWEEN ELEVATOR STATION 99.50-136.50 DISPLACED UPPER ELEVATOR SKIN FROM BS 99.5 TO BS 136.5 IAW SRM 51-30- 02 AND REMOVED REPAIR DOUBLER FROM LOWER SKIN. HFEC CARRIED
- [SDR UPS06247053](https://openairdocs.org/sdr/UPS06247053.md): Rib · cracked · May 23, 2006 · N944UP · Boeing 72722C · Elevator, Spar/Rib
  > INSPECTION TYPE:C X-RAY INSP DETECTED ONE SUSPECT CRACK ON THE LT ELEVATOR INTERNAL RIB LOCATED BETWEEN ELEV STA 179.50 - 205.50. ELEV BEYOND ECONOMIC REPAIR REF NRC 100783 FOR REPLACEMENT OF LT ELEVATOR.
- [SDR UPS06247056](https://openairdocs.org/sdr/UPS06247056.md): Casting · cracked · May 19, 2006 · N944UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C LEFT O/B FOREFLAP I/B SECTION HAS CRACKS FROM FASTENER HOLES. PAINT STRIPPED AREA IAW MM 51-20-01. HFEC INSP CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. RESULT - CRACK CONFIRMED. FOR FLAP REPLACEMENT REF NRC 100295 DUE TO I/B CASTING N
- [SDR UPS06247046](https://openairdocs.org/sdr/UPS06247046.md): Skin · delaminated · May 18, 2006 · N944UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE:C NR 9 SPOILER DELAM ON LOWER SURFACE AT O/B FWD CORNER. DELAMINATED SKIN REMOVED AT O/B FWD CORNER IAW SRM 51-40-20. DELAM LIMITS FOUND TO BEYOND ECONOMIC REPAIR. SPOILER REPLACED.

Next page: https://openairdocs.org/model/boeing-727-22c/reports.md?page=2

## 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 aircraft_model_key = '72722C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-22c/reports

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